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A STUDY OF LIGHT RIGID ROTOR NUCLEI - Wright Laboratory · 2019. 12. 20. · Mg28(p,o!'y)Na28,...

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296
by Richard A. Lindgren B.A. , University of Rhode Island, 1962 M.A. , Wesleyan University, 1964 A STUDY OF LIGHT RIGID ROTOR NUCLEI A Dissertation Presented to the Faculty of the Graduate School of Yale University in Candidacy for the Degree of Doctor of Philosophy 1969
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  • byRichard A. Lindgren

    B.A. , University of Rhode Island, 1962

    M.A. , Wesleyan University, 1964

    A STUDY OF LIGHT RIGID ROTOR NUCLEI

    A Dissertation Presented to the Faculty of the

    Graduate School of Yale University in

    Candidacy for the Degree of

    Doctor of Philosophy

    1969

  • To my Family

  • The author would like to thank his graduate research adviser,

    Professor D. A. Bromley, for the opportunity to carry out this work, for

    his inspirational advice, for his encouraging suggestions, and especially

    for his constructive criticism in the preparation of this manuscript. These

    moments will long be remembered.

    I also would like to thank Drs. J. G. Pronko and A. J. Howard for

    continued interest and thought-provoking discussions on this work and

    many related matters. The author also wishes to acknowledge Dr. M. W. Sachs

    for his consultation in computer programming and m y student colleague,

    Dr. R. G. Hirko for his assistance and participation in numerous aspects

    of this work. The stimulating discussions with and assistance from other

    graduate students will always be remembered.

    The author thanks the entire technical staff of the A. W. Wright

    Nuclear Structure Laboratory, whose individual assistance and coordinated

    efforts are greatly appreciated.

    I sincerely thank m y family, in particular, m y wife, Ruth, and

    children, who have endured without complaint m y negligence as a husband

    and father.

    The United States Atomic Energy Commission is gratefully

    acknowledged for its financial support of this entire research.

    ACKNOWLEDGEMENTS

  • ABSTRACT

    In an attempt to empirically determine the degree to which the concepts of the simple rigid rotor model approach to light collective nuclei is valid, a study of four similar; strongly deformed, prolate nuclei in the odd count £ = 11 nuclear multiplet has been undertaken. Two members of this multiplet, Na21 and Na22, have been studied utilizing the M g 24(p,Q!'y'Na21, M g 28(p,o!'y)Na28, M g 24(t,o('y)Na22, and Na22(ry, a* y)Na2 reactions in the standard Method n angular correlation geometry of Litherland and Ferguson.

    N e w angular m o m e n t u m quantum numbers and electromagnetic de-excitation properties have been determined for levels and transitions in these nuclei. These data together with works of others have been systematically examined by comparing model predictions based on the rotor, Coriolis, and shell models with experiment for the Ne21, Na21, Na22, and M g 22 odd count £ = 11 nuclei.

    W e have determined from these comparisons that the rotor and Coriolis model predictions of excitation spectra, electric quadrupole and magnetic dipole reduced transition probabilities in the K ff= 3/2+ ground state rotational band in the £ = 11 nuclei are in better agreement with experiment than the shell model results. Further, the Coriolis results including other single particle configurations reproduce the magnetic dipole transitions matrix elements better than the pure rotor model calculation. Both models, rotor and Coriolis, are equally as effective in reproducing the electric quadrupole transitions as would be expected in a well deformed nuclear system. ^

    Despite the remarkably accurate predictions of the electromagnetic transition properties by the simple rotor model in this multiplet, validating the use of the model, there still remains an unexplained oscillatory pertur- bative deviation of the excitation energies from the J(J+1) rule in the mirror pair Na22 and M g 22. Although only partially confirmed, a Coriolis based explanation appears appropiate to correct this anomaly as is seen by the improvement of the Coriolis model over the rotor model in reproducing the excitation spectra of the ground state rotational band.

    The large, almost limiting, rigid body values of the moment of inertia (>90%) and the strong prolate nuclear deformations ( 8 ~+0.5), completely supporting the premises on which the rigid rotor model is based, characterize the odd count £ = 11 group of collective nuclei without exception as perhaps the most rigid rotors in nature.

  • TABLE OF CONTENTS

    Abstract

    A cknowledgements

    Introduction.................................................. 1

    A. Motivation............................................ 1

    B. General Considerations............................... 2

    1. Model overlap..................................... 2

    2. Evidence for collectivity............................ 4

    3. Limitations of collectivity.......................... 5

    C. Nuclear Models....................................... 9

    1. The strong coupling collective m o d e l ............... 9

    a. The Nilsson m o d e l.............................. 13

    b. The Hartree-Fock method...................... 14

    c. The Coriolis coupling model.................... 15

    2. The shell m o d e l ................................... 17

    a. The extreme single particle shell m o d e l ....... 17

    b. The single particle shell m o d e l ................. 18

    c. The individual particle shell m o d e l ............. 19

    3. The SU m o d e l ................................... 2123

    D. Literature Survey on Model Interpretations of N a ....... 2321 23

    E. Rotational Structure of Na and Na .................... 26

    1. Rotor behavior..................................... 26

    2. Nuclear rigidity................................... 29

    F. Rotational Perturbations................................. 31

    1. Nonconstant moment of inertia.................... 32

    2. Higher order Coriolis perturbations............... 34-2

    3. Expansion of Hamiltonian in powers of R ......... 36

    4. Wave function admixtures............................ 39

    G. Model Comparison Using Electromagnetic Properties . . . 41

  • H. Experimental M e t h o d ..................................... 42

    1. G a m m a ray angular distribution from aligned nuclei. 43

    2. Reactions......................................... 44

    3. Background radiation difficulties.....................45

    I. S u m m a r y .................... 46

    n. Apparatus.................................................... 48

    A. Accelerator.............................................. 48

    B. B e a m Transport......................................... 50

    C. G a m m a Cave and Goniometer............................ 51

    D. Radiation Detectors......................................... 51

    E. Associated Components................................... 52

    1. Scattering c h a m b e r ............................... 52

    2. Detector shield.......................................53

    3. Detector cooling................................. 54

    4. Electron shielding............................... 54

    5. Faraday c u p ....................................... 55

    6. B e a m stop......................................... 5623 24 26

    F. Preparation of N a , M g , and M g Targets........... 56

    G. V a c u u m .................................................. 57

    H. Electronics................................. 58

    I. Hardware . . . ........................................... 59

    J. Software................................................ 8°HI. Data Acquisition........................................... 81

    IV. Data R e d u c t i o n ............................................ 85

    V. Data Analysis . . .......................................... 89

    A. Method n Angular Correlation F o r m a l i s m ...................69

    B. Spin Assignments and Rejection Criteria................. 73C. Mixing Ratios............................................ 79D. Finite Solid Angle Effect (FSE)............................ 75

    VI. Experimental Results...........................................7723 23 77

    A. N a faa1 y)Na ......................................... 7726. ,XT 23 7q

    B. M g (p,o! y)Na .........................................

  • vn.vm.

    ix .

    „ 2 4 23C. M g (t,ay)Na ......................................... 8224 21

    D. M g (p,a y)Na ......................................... 82

    Discussion of Results....................................... 84

    Summary of Results on Odd Count £ = 11 Nuclei.............. 999 Q

    A. Na .................................................... 99

    B. N a 21.................................................... 1009 1 9 9

    C. Ne and M g ......................................... 101

    Model Interpretations of Odd Count £ = 11 N u c l e i .......... 102

    A. Collective model interpretations of K ff=3/2+ ground state

    rotational b a n d ........................................... 105

    1. Rotor model predictions with Nilsson intrinsic wave

    functions......................................... 106

    a. Excitation energies, branching and mixing ratio. 106

    b. Intrinsic quadrupole moments and gyromagnetic

    ratios......................................... 109

    2. High order Coriolis and rotational perturbations. . 114

    3. Coriolis coupling m o d e l .......................... 115

    a. Excitation energies.......................... 115

    b. Electromagnetic properties................... 120

    1. Absolute reduced matrix element comparisons 120

    2. Relative comparisons...................... 122

    B. Rotational B a n d ................................ 124

    1. Asymptotic selection r u l e s ........................ 125

    2. Calculation of El transitions.................... 128

    3. Band purity.............. 129

    C. Sensitivity of Electromagnetic Properties to the Nuclear

    Deformation.............................................. 130

    1. Coriolis coupling model predictions............... 130

    2. Inelastic scattering of particles.................. 131

    3. Direct measurement from electromagnetic properties 131

  • D. Other Nuclear Model Predictions......................... 136

    1. Excitation energies............................... 136

    2. Electromagnetic properties........................ 137

    a. Static comparisons.............................. 137

    b. Dynamic comparisons.......................... 137

    X. S u m m a r y and Conclusions.......................................140

    References............................. 142

    Appendix I .................................................... 149

    Appendix II.................................................. 155

    Appendix III.................................................. 159

    Appendix I V .................................................. 161

    Appendix V . .............................................. 165

    Appendix V I ................................................. 179

    Appendix V I I ................................................ 182

  • The complexity of the interactions between nucleons of a nuclear

    system precludes a rigorous mathematical treatment of nuclei in terms

    of fundamental internucleon forces, especially in view of our insufficient

    knowledge of the force producing meson-exchange fields. Even if these

    force fields were precisely known, however, we would not be able to solve

    the nuclear problem, since state of the art mathematical techniques are

    not capable of handling the many body problem in any exact fashion; Not

    only are we uncertain of the nuclear forces and limited in our mathe

    matical framework, but application of nonrelativistic Schrodinger quantum

    mechanics to interactions confined to subnuclear dimensions is not

    entirely correct, in the light of marginally important relativistic correc

    tions necessarily imposed by Heisenberg’s Uncertainty Principle. However,

    such corrections are small and assumed to have a negligible consequence

    on the main body of nuclear structure.

    Within the Schrodinger formalism the unknown nuclear forces and

    unsolvable many body problem are avoided by constructing solvable models

    whose salient features approximate the nuclei of interest and the physical

    properties of which can be calculated explicitly for comparison with

    experiment. The success of this approach is measured by the inherent

    plausibility of the selected model and by the degree of agreement attained

    I. INTRODUCTIONA. Motivation

  • 2

    between theory and experiment, not only for any given nucleus, but also,

    and more importantly, for groups of systematically selected nuclei

    spanning related areas in the periodic table. F r o m such models certain

    basic underlying features emerge, which must necessarily be incorporated

    into any fundamental understanding of nuclear structure and behavior. It

    seems probable that major improvement in our understanding of the

    nucleus will occur in such an empirical and phenomenological manner.

    B. General Considerations

    1. Model overlap

    Since the successful application of the strong-coupling

    collective model to light nuclear systems (Br 57, Li 58), nuclei in the

    mass region 19 ̂ A ̂ 2 5 have been of growing experimental and theoretical

    interest. Additional and more extensive studies, including the present

    work, have definitely established nuclear collectivity in this mass region

    (Ho 65, P o 66, D u 67, Pr 67, Pr 69a). These nuclei possess strong, rigid

    prolate deformations with rotational structure of varying degrees of

    purity and relatively large moments of inertia, greater than 90% of rigid

    body values in some cases.

    Early shell model calculations in the sd shell were first applied

    to the mass 18 and 19 nuclear systems (El 55) and, recently, more realistic

    shell model calculations have been applied to nuclei throughout the mass

    region defined above (Bo 67, H a 68, Wi68). Although the shell model features

    are not as prominent as the collective ones, the excitation spectra can be

  • 3

    well reproduced, if appropriate amounts of configuration mixing in the sd

    shell is included; wave functions from such calculations, however, have

    not been thoroughly tested. Comparison of the results of applying these

    various models to similar nuclei has already led to a much improved

    understanding of nuclear behavior and to isolation of the more fundamental

    aspects of the nuclear problems involved.

    As an example, Elliott (El 58), in reproducing collective behavior

    19in F by expanding over appropriately selected shell model wave

    functions, developed the SU Coupling Model, in which wave functionsOwere classified according to the symmetries of the special unitary group

    in three dimensions (SU ). This model has been applied with moderateOsuccess in the first half of the sd shell (El 62, El 67, Ha 68a) and has

    resolved what had for some time appeared to be rather fundamental dif

    ferences between the apparently equally successful shell and hydrodynami-

    cally based collective models.

    The mass region defined herein is basically, as yet, the only

    region containing a sufficient number of nuclei which exhibit pronounced

    collective behavior to permit a detailed systematic study in terms of the

    collective model, yet with few enough extra-core nucleons involved to

    permit treatment within the framework of the shell model. This situation

    is unique in defining a testing ground overlapping the region of applicability

    of three major nuclear models, collective, shell and SU^, which can now

    be directly compared; such comparisons had not been exploited in full

  • 4

    detail in the past for lack of adequate precise nuclear spectroscopic

    information on the nuclei involved. By systematic comparison of the nuclei

    spanning the aforementioned mass region in terms of dynamic as well as

    static nuclear nuclear properties, we hope to gain a more fundamental

    understanding of the behavior and symmetries of nuclear systems and of

    the interrelationship of these nuclear models.

    2. Evidence for collectivity

    Within the collective framework, the strong-coupling model

    based on Nilsson intrinsic states (Ni 55) has been applied to odd A nuclei

    in the mass region 19 ̂ A ^25 with overwhelming success in comparison

    to the often mediocre results obtained with the shell and SU^ models. Not

    only has it been successful, but also the simplicity with which calculations

    can be performed and compared with experiment has made it the most

    popular mode of data interpretation in this mass region.

    The model consists of a single extra core nucleon coupled to a

    rigid, well-deformed core. The interaction between the orbiting particle

    and the core is represented by a deformed simple harmonic oscillator

    potential which is discussed in more detail in section I-C.

    The early, macroscopic collective models typically parametrized

    experimental data in terms of physically meaningful quantities such as

    the moment of inertia, nuclear deformation, etc. A systematic study of

    the evolution of these parameters throughout a major shell (sd) can yield

    valuable nuclear structure information regarding the rigidity and shape of

  • 5

    the nucleus and, indirectly, the importance of the various components of

    the nuclear force as the shell fills (Hi 69). A plot of the moment of

    inertia obtained as a parameter in fitting the ground state rotational bands

    of available nuclei according to the crude rotor equation, E = A J(J+D,

    2where A = ft /2I, is shown in Fig. 1. It should be noted that I for a rigid

    2 2 spheroid is given (Bo 55) by I = 2/5 M R (1 + 0. 31 8+ 0. 44g + . . .) and

    that it is, therefore, a relative measure both of the deformation gand of

    the rigidity of the nucleus; it is clear from this figure that the apparent

    deformation maximizes in the region defined by the mass 21, 22, and 23

    nuclei.

    More conclusive evidence for rotational behavior in this region is

    signified by enhanced intraband E2 matrix elements, which are shown in

    Fig. 2, plotted in Weisskopf units versus the atomic weight of the nucleus

    involved. Rotational enhancements are again most marked for these same

    nuclei. W e have, herein focussed our attention on these nuclei comprising

    the region of m a x i m u m deformation and rigidity, within the sd shell; this

    has been done in the hope of testing the extent to which the apparent collec

    tive characteristics m a y be extrapolated before the simple concepts on

    which they are based require modification.

    3. Limitations of collectivity

    Of particular interest in this work is the class of odd A

    collective nuclei, whose last odd nucleon is the eleventh located in orbit

    7 (K77 = 3/2+) of the Nilsson model. This defines the nuclear multiplet of

  • 10

    9

    8

    7

    6

    o 5I / f l

    4

    3

    2

    I

    18 2 0 2 2 2 4 2 6 2 8 3 0ATOMIC MASS NUMBER

    M O M E N T OF IN E R T IA V E R S U S A T O M IC M A S S

    * 2A = n / 2 I A Is a parameter determinedby a least squares fit to the ground state rotational band

    I i I l I I I I I 1-------1-------1------ L

    Fig. 1

  • |M|

    FOR

    E2 Q0

    (bar

    ns2)

    ATOMIC WEIGHTF ig. 2

  • 6

    Ne , Na , Na , and M g categorically referred to as the odd count

    £=11 nuclei. On the basis of the most simple (single particle) Nilsson

    model interpretation these nuclei should exhibit indistinguishable nuclear

    structure. In search for rotor behavior among these nuclei we have found

    an unexpected marked difference in the sequence of excitation energies of

    21 21the ground state rotational bands for the mirror pairs (Ne , Na ) and

    23 23(Na , M g ) with the latter pair manifesting distinct departures from the

    almost pure rotor behavior exhibited by the former pair (Fig. 3). In

    contrast the g a m m a ray de-excitation properties are in relatively good

    agreement with rigid rotor behavior for both mirror pairs of nuclei. This

    is rather surprising in that dynamic properties are usually more sensitive

    to wave function admixtures, and small departures in predicting excitation

    energies usually result in larger departures in predicting transition

    probabilities. A detailed account of this anomaly is deferred until more

    general considerations are discussed.

    Two other known nuclei that fall in the £ = 11 nuclidic category, but

    are best described in terms of the shell model, as verified by the predicted

    ground state spins of 5/2 in contrast to the collective prediction of 3/2 for

    19 25the aforementioned nuclei, are O and Na . Although these nuclei are

    not specifically considered in this work, they are important in that they

    border the concerned region of collectivity reflecting the dependence of

    the nuclear deformation on isospin and subshell closure. As an illustra

    tion of this dependence, the mean square deviation of the excitation energies

  • E(M

    eV)

    E(M

    eV)

    E X C IT A T IO N E N E R G Y V E R S U S J(J + I)

    7.06.05 .04 .03.02 .0 1 0

    6.450-

    4.431-

    2.867-

    1.747-

    .3 5 0 - *- 0N e 2 i

    J (J+1)

    7.06.05 .0 4 03.02.0

    1.0

    2 .705- h 2 .079-

    .4 3 90

    No 2 3 J(J + I)F ig. 3

  • 7

    from the calculated values determined by a least squares fit to the ground

    state rotational band members by the equation E = A(J)(J+1) for Ne, Na,C c t iC

    and M g isotopes, is plotted versus atomic mass number in Fig. 4. For each

    isotopic group there exist optimum rigid rotor behavior characterized by

    the minima of the parabolic curve drawn through a given isotopic sequence.

    This apparent simple parabolic dependence of rigid rotor behavior

    on neutron occupation number is rather remarkable considering the c o m

    plexity of the deformation-reducing short range pairing forces, competing

    long range forces tending to align nucleonic orbitals maintaining deformation,

    and subshell closure effects. A discussion of these effects can be found

    in references Br 60, M o 60, Ro 67a, and Bo 69.

    In this region, where nuclei m a y well be among the most rigid in

    the periodic table, an addition or subtraction of a proton or neutron

    markedly effects the rotational character as is seen by the sharpness of

    the slopes and narrowness of the curves shown in Fig. 4. In light of this

    the differences between the relative location of the band members with

    respect to rotor model predictions shown in Fig. 3, which are unexplained

    on the basis of a macroscopic model, is not then surprising.

    These differences are a result of the fact that nuclei are obviously

    not perfectly symmetric rigid bodies with well defined nuclear surfaces.

    Even in regions where the model works best there are unexplained systematics

    and discrepancies between theory and experiment. A particularly interesting

  • 1 0 ° O’ 2 V E R S U S A T O M IC M A S S

    o ' 2 * 4 * I

  • 8

    example of this has very recently appeared in the measurements of the

    20 22intrinsic quadrupole moments of certain even A nuclei such as Ne , Ne ,

    24 +and Ne in this mass region, when in their first excited 2 states (Ha 68a,

    Na69, Sc 69, Sc 69a). These measurements have yielded the very

    surprising results that these states have quadrupole moments 30% greater

    than those which would be expected for rigid rotors having the experi

    mentally determined deformation of the 0+ ground states in each case.

    Not only are these results in themselves not yet understood, but also the

    contrast between these nuclei and the adjacent odd mass isotopes, as

    studied herein, is most striking.

    These seemingly inexplicable disagreements are, of course,

    manifestations of many unaccounted for degrees of freedom intrinsic to

    the microcomposition of the nucleus. In search for possible explanations

    of these departures from pure collectivity, we have concentrated on

    examining, systematically, the static and dynamic properties of this

    group of nuclei in terms of the present strong coupling Nilsson model and

    in terms of possible extensions and modifications thereof incorporating new

    and previously unaccounted for degrees of freedom. In this way we have

    attempted not only to explain present disagreements, but also to determine

    the limitations of the simple collective approach.

    To put this problem in perspective, a brief review of nuclear

    models is presented emphasizing aspects of each according to their

  • 9

    importance in the work discussed herein.

    C. Nuclear Models

    1. The strong coupling collective model

    The strong coupling collective model of Bohr and Mottelson

    (Bo 52, Bo 53) as applied to odd A nuclei consist of a rotating deformed

    core with angular momen t u m R coupled to a single extra-core nucleon

    orbiting about the core with angular m o m e n t u m j (Fig. 5). The total

    angular m o m e n t u m J of the core plus particle is given by

    J = R + j .

    The Hamiltonian in the strong-coupling model framework m a y then

    be written as

    h = a r 2 + h 'sp

    —►2where A R is the rigid rotor contribution from the core, A is the moment

    2 /of inertia parameter h /2I, and H^ is a single particle Hamiltonian

    representing the interaction of the single odd nucleon with the core. Since

    2R is not a constant of the motion, it is more useful to substitute

    R = J - r,

    expand the square (J- j )2 and dot product (J • j ) obtaining,

    H = A J 2 - 2AJ3i3 - 2A(J1j1 + J2y +Aj*2+ ff'p .

    Since the core is assumed, in this simple model, to be axially symmetric,

    the projection of R on the body-fixed symmetry axis is zero (Rg=0).

    Using the notation K=J0 and (1= j and substituting R =0 in the equationu O O

  • STRONG COUPLING MODEL PICTURE OF ODD A NUCLEI

    z

    F ig . 5

  • we find K = Q. That is, the projection of the total angular m o m e n t u m on

    the symmetry axis is equal to the corresponding projection of the angular

    m o m entum of the orbiting single particle outside the core and is a constant

    of the motion in the absence of the familiar Coriolis coupling of intrinsic

    and rotational motion in such a system.

    By defining ladder operators in the usual fashion,

    J ± = J l± i J 2

    for the components of J and j, substituting into the expression J j + J j ,JL J. d dand rearranging terms, the Hamiltonian in the strong coupling model m a y

    be written in the form

    H = H + H + H , rot cor sp

    where

    H 4 = A(J2 - 2K2) , rot

    Hcor = 2A(J+i- + J> >

    and H = A j 2 + H' .sp sp

    2The core Hamiltonian A R has been subdivided into a pure rotational

    part H and a part H coupling the rotation of the core with the single rot cor

    extra-core nucleon in analogy with the form of the classical Coriolis

    rotational coupling term co* j . The last component, H , is a generalsp

    single-particle Hamiltonian whose specific form is dependent on the choice

    of interaction between the odd particle and the core.

  • 11

    By neglecting the Coriolis coupling terms we may write the

    Hamiltonian as

    H = ft2/2I ( J ^ K 2) + H .sp

    Without specifying the exact form of and restricting ourselves to

    deformed axially symmetric nuclei, the Hamiltonian may be conveniently

    diagonalized in a basis defined by eigenfunctions of the form (Da 69)

    where are single particle intrinsic eigenfunctions of H ,D^_ (0 .)Sp lv i.1 V 1

    are rotation matrices of Euler angles (0 .), and C _ a r e expansion

    coefficients. The wave function | J K M > is characterized by total momentum

    J with projections on the body fixed and spaced fixed axes of K and M,

    respectively.

    This form of the wave function is characteristic of the strong coupling

    model and does not depend on the specific choice of H gp« The two part

    wave function depending on K and -K is a result of the axial symmetry of

    the core and it is just this symmetry that is responsible for diagonal

    contributions to the Hamiltonian from the Coriolis coupling terms in the

    case of K=l/2 bands and in higher bands when correspondingly higher order

    powers of the Coriolis perturbation are included. F r o m this simplified

    form of the Hamiltonian it follows that for relatively large moments of

    inertia the model predicts a series of closely spaced rotational levels

    built on more widely spaced single particle levels. The faster orbiting

  • 12

    single particle "follows" the slower rotating core with no significant

    perturbation of the orbit of the single particle (adiabatic approximation).

    In heavy odd A nuclei, where I is large enough to validate

    this assumption, the Coriolis coupling can be by and large safely

    neglected. In contrast to the heavy nuclei, the smaller moments of

    inertia of light nuclei, although almost rigid body values, cause complete

    overlap of single particle and rotational levels in violation of the adiabatic

    approximation. In spite of this violation, rotor-like spectra surprisingly

    22have been still identified. In some cases such as Na the absence of

    nearby rotational bands satisfying the K band mixing selection rule £K=±1

    21preserves the rotational structure, while in other nuclei such as Ne ,

    23Na , etc. no equivalently simple explanation has been presented to account

    for the preservation of the ground state rotational bands in the presence

    of possible full Coriolis coupling.

    Before specifying H gp> follows from the form of the wave function

    that the calculation of any dynamic properties linking levels in a given

    rotational band depends solely on the properties of the rotation matrices,

    since the intrinsic parts of the wave function remain unchanged. This is

    an extreme simplification and comparison of predicted and experimental

    E2 transition strengths have provided characteristic signatures for

    rotational behavior as have the large static ground state quadrupole

    moments observed in these cores.

    The band heads are not confined to single particle origin. In even-

  • 13

    even nuclei H is replaced by a vibrational Hamiltonian (Bo 53) where the

    nucleus is assumed to undergo vibrations similar to those of a liquid drop.

    The Coriolis coupling term is replaced by an analogous term coupling the

    rotations and vibrations of the nuclear surface. Applying the adiabatic

    approximation to this model and likening the vibrational motion to the

    single particle motion, rotational levels are built on vibrational band

    heads denoted as beta (axial vibrations) and g a m m a (nonaxial vibrations)

    bands. Rotational bands of this nature are c o m m o n in rare earth and

    actinide nuclei, but have not as yet been found, unambiguously, in light

    sd shell nuclei.

    a. The Nilsson model

    To obtain further detail from the strong coupling

    model the form of H gp must be specified. In light odd A nuclei the most

    simple and successful approach has been the Nilsson Hamiltonian (Ni 55)

    in the form

    h = h + cT- r + dT- rN o

    where

    Ho = l b + t maJo r2 f1- 2 ̂Y2 0 ^ ) -

    H q is a single-particle deformed harmonic oscillator potential with

    deformation 0 , characteristic mass m, and frequency coQ . S and I are the

    intrinsic spin and orbital angular m o m e n t u m of the particle, and C and D

    2are parameters measuring the strength of the spin-orbit and L terms,

    respectively. The form of these latter terms is given by the comparison

  • 14

    has shown that the coefficients there derived are not physically realistic;

    hence C and D have been introduced as fitting parameters in the model.

    The result of diagonalizing the Nilsson Hamiltonian is a sequence

    of single particle deformed orbitals which are functions of the nuclear

    deformation ]3. The constants C and D were originally chosen to give the

    appropriate shell model level splittings in the limit of zero deformation.

    A typical Nilsson energy level diagram is shown in Fig. 6 illustrating the

    23filling of the single particle orbits of Na for a given deformation

    3 B 5(T) = / — ). The total Hamiltonian that is diagonalized in the strong

    coupling Nilsson model is

    H = A(J 2) + H n

    where the Coriolis coupling term has been completely neglected. Application

    to light nuclei in the sd shell, particularly in the first half of the shell,

    has been surprisingly successful (Li 58, Ho 67, Po 66, Pr 67), especially

    in light of the non-fullfilment of the adiabatic approximation. Where

    necessary the Coriolis interaction has been introduced as a perturbation

    operator using the eigenfunctions of the above Hamiltonian as a basis

    set.

    b. The Hartree-Fock method

    In an attempt to determine a more general set of

    single particle deformed orbitals Levinson and Kelson (Ke 63, Ke 64)

    employed a Hartree-Fock variational method leading to a Hamiltonian that

    of the j term appearing in the above R expansion, how ever, experience

  • V

    Fig. 6

  • 15

    included a harmonic oscillator part plus spin orbit and -T terms and a

    two-body Rosenfeld interaction having a Yukawa radial dependence. The

    strength of the two body interaction was used as a parameter and serves

    in a capacity similar to the nuclear deformation in the Nilsson model. The

    calculated positions of the single particle orbits are similar to those of

    Nilsson and the results only differ substantially in the placement of hole

    excitations. In the Hartree-Fock calculations the hole excitations are

    consistently located higher in excitation than in the Nilsson case. The

    large gap between filled and unfilled orbitals reflects the inclusion of

    exchange forces in the Hartree-Fock Hamiltonian, which are absent in the

    Nilsson case. This is a vitally important aspect of the nuclear many body

    problem analogous to that characteristic of the superfluid and super

    conducting states in the theory of condensed matter.

    c. The Coriolis coupling model

    The nuclei under discussion are filling sd subshells

    16outside an assumed inert core of O . Rotational bands are based on

    single particle or hole excitations where the former are generated by

    promoting the last odd nucleon to higher lying orbit s previously illustrated

    in the Nilsson energy level diagram in Fig. 6. Hole excitations differ

    in that the nucleon is promoted from a fully occupied lower lying orbit to

    a previously partially occupied higher lying one. Within the sd shell there

    are six possible positive parity orbits into which a given nucleon can be

    excited including, in the case of the odd count £ = 1 1 nuclei, a hole

  • 16

    1T +excitation based on a K =1/2 band derived from the d . subshell.

    5/2

    Low lying negative parity states have also been, heretofore,, identified

    as hole excitations originating from the lower fully occupied p shell.

    In the simple rotor or Nilsson model, interactions between the single

    particle or hole levels are ignored. This approximation is justified if

    the interacting band heads are much further apart than are the rotational

    23levels within any given band. For most levels in Na this criteria is not

    satisfied and proper account of these interactions is accomplished by

    including the Coriolis term in the total Hamiltonian.

    The most consistent and complete treatment of Coriolis band

    mixing in the sd shell has been developed in the Coriolis Coupling model

    of Malik and Scholz (Ma 67). Here the total Hamiltonian to be diagonalized,

    in the sd shell subspace, is written as

    H = H a+ H + H rot cor sp

    where H H , and H have been previously defined as the rotor,rot cor sp

    Coriolis Coupling, and Nilsson terms, respectively.

    The single particle band heads are calculated from the equation

    (Ne 60)

    E = £ +£ r > r+ D t.-fc -where E is the Nilsson energy of the individual nucleons and the sum»£> Vis over all nucleons in the nucleus. M is the true nucleon mass and p is

    an effective mass defined by Newton (Ne 59). The parameters A, |3, C,

  • and D are varied until the best fit between the calculated energy levels

    and the experimental ones is obtained.

    The range of the parameter C is restricted to values that lie

    17 39between the d 5/2- d 3/2 level splitting of O and of Ca in the limit

    of zero deformation. Using this model, generally good fits have been

    obtained systematically for sd shell nuclei with reasonable sets of para

    meters (Ma 67, Hi 69).

    2. The shell model

    In contrast to the simplicity with which the collective model

    m a y be applied to light nuclei in the sd shell, the complexity of realistic

    shell model calculations requires the use of high-speed, large-memory

    computers to perform large matrix diagonalization even for a system of

    a few active nucleons. These calculations have been prohibitive in the

    past and only because of the recent availability of such computers has it

    become possible to treat nuclei in this framework.

    a. The extreme single particle shell model

    Simple shell model treatments are completely

    inadequate as m a y easily be demonstrated by attempting to predict the

    + 23anamolous 3/2 ground state spin of Na on a shell m o d e l basis.

    In the extreme single particle shell model of odd A nuclei, the nucleus is

    approximated by a single particle moving in a potential well given by

  • 18

    where V(r) is a central potential, the behavior being intermediate between

    a square and a simple harmonic oscillator well, and -t and s are the orbital

    and spin angular momenta of the single particle. This model, enunciated

    by Mayer (Ma 50), which correctly predicted the ground state spin of

    23almost all stable nuclei, incorrectly predicted a 5/2 assignment for Na , the

    55only other major discrepancy at the time being M n . In view of this,

    application of a limited shell model to these nuclei should be with parti

    cular reservation.

    b. The single particle shell model

    A slightly more sophisticated approach involves

    incorporation of a residual interaction between the nucleons outside a

    closed shell, but not so strong that it cannot be treated by first order

    perturbation theory. This approximation is called the single particle

    model (Pr 62) where the total potential of the extra core nucleon can be

    schematically written as

    H = £ V(r.) + L At.* s. + T v(r..)sp i i' i i i i

  • 1 9

    c. The individual particle shell model

    This rule no longer applies and the ground state spin

    23of Na is correctly predicted when including strong residual interactions

    (FI 54, El 55) between the extra core nucleons especially in cases where

    configuration mixing includes the s 1 y 2 and d3/2 orBits as w e R as tlie % / 2

    (Bo 67, Wi 6 8). In this approach the Hamiltonian differs from that of the

    single particle model in that the strength of the residual interactions is

    stronger, requiring a total diagonalization of the Hamiltonian, since

    neither LS nor jj coupling are diagonal representations of the perturbations.

    W e refer to this approach as the individual particle model or intermediate

    coupling model. Reasonable agreement for the energy levels up to 4. 0 M e V

    23in Na , as well as in other sd shell nuclei, were obtained in the calcula

    tions of Bouten et al. (Bo 67) performed within the framework of this

    model. The technique consisted of calculating excitation spectra in the

    two extremes of LS and jj coupling and using first order perturbation

    theory to calculate small departures from each extreme as a function of

    the strength of ts coupling. Assuming that the eigenvalues are smooth,

    monotonic functions between the two extremes, energy eigenvalues for

    arbitrary degrees of intermediate coupling were then obtained by inter

    polation. The approximation appears to be valid for eigenvalue inter

    polation, but fails in calculating wave functions which are necessary for

    calculation of any of the electromagnetic dynamic properties.

    single particle model.

  • 20

    Another approach, taken by Wildenthal et al. (Wi 68), applied to

    20

  • 21

    perform the calculation. Therefore, the actual nuclear wave function is

    approximated by the expansion functions, but in certain cases the

    approximation is quite good.

    19In the specific case of F , both the shell and collective models

    gave a reasonable fit to the energy levels and, indeed, it was observed

    that rotational behavior could be derived by expanding over a limited

    number of shell model configurations (El 58). This initiated the

    application of group theoretic techniques to the classification of nuclear

    energy levels. This has the advantage of exploiting the nuclear symmetry

    through the transformation properties of orbital angular m o m entum eigen

    functions.

    3. The SU modelOIf a given Hamiltonian is invariant under the symmetry

    operations of a group, then there corresponds to each eigenstate of the

    Hamiltonian an irreducible representation of the group, by which the eigen

    state m a y be labelled. The degeneracy of the eigenstate is given by the

    dimensionality of the group.

    Elliott (El 58) showed that the symmetry group of the three dimen

    sional harmonic oscillator Hamiltonians is the special unitary group in

    three dimensions (SU~). Therefore, the eigenstates of the harmonicOoscillator Hamiltonian can be labelled according to the irreducible repre

    sentations of the SU group. Assuming the radial dependence of theOnuclear Hamiltonian is dominated by harmonic oscillator like terms leading

  • 22

    to a long range effective force of the r. r P 2(cos0„) type and that spin-

    orbit coupling or spin-dependent forces are negligible, then SU will beuan approximate symmetry group of the nuclear Hamiltonian. Because of

    the principle of indistinguishability of identical nucleons comprising a

    nuclear system, the Hamiltonian must also be invariant under the permu

    tation group. Since SU and the permutation group operate in differentOspaces, eigenstates of the Hamiltonian can be simultaneously classified

    according to the irreducible representations of each.

    A class of states possessing particular permutation symmetry,

    determined in part by requiring the total wave function to be antisymmetric,

    m a y be labelled by a partition [f] and then, for a given partition, the

    individual eigenstates of the class are labelled by the SU quantum numbersO(X,pi) in addition to the usual L,S,T,etc. quantum numbers. The lowest

    lying states are labelled by irreducible representation (A, p ) that correspond

    to states of m a x i m u m orbital symmetry with X " ^ > p corresponding to prolate

    shapes and \ « p corresponding to oblate shapes.

    23In Na the lowest lying positive parity states are classified

    according to the partition [43] with the (8,3) leading representation of S U g(Ha 68a).

    For non-zero ground state intrinsic spin nuclei the intrinsic state or

    leading representation contains more than one eigenstate of the same J.

    The " J projection scheme" is used to classify states of the same J

    according to their K labels. In the example given K = 1/2, 3/2, 5/2, and

    7/2 and for each K, J = K, K + 1, . . . K + A. Indeed, K = 1/2, 3/2, and

    2 2

  • 23

    23 TT +5/2 rotational bands have been identified in Na . In the K = 3/2

    23 +ground state band of Na , members up to the = 13/2 level inclusive

    have been identified, but not as yet has the predicted cutoff of J n = 19/2+

    19 i t +been reached. In F members of the ground state K = l/2 band are

    __ .j.known up to the J = 13/2 SU predicted cutoff limit and at this time noOvalues are known which exceed the SU limit. It would clearly be of greatOinterest to firmly establish the validity or breakdown of these SU_ predic-Otions in the form of higher spin band members. As yet the only discrep-

    g

    ancy is the rather special one in Be .

    23D. Literature Survey on Model Interpretations of Na

    23The earliest attempts at calculating the low lying spectra of Na

    were done with the collective model. The calculations of Litherland (Li 58),

    Rakavy (Ra 57), Paul and Montague (Pa 58), and of Clegg and Foly (Cl 61)

    were performed with Coriolis coupling included in the strong coupling

    Nilsson model. Moments of inertia and band head excitations were used

    as parameters in obtaining fits for the first three excited states. The

    lack of definitive experimental spectroscopic information discouraged any

    detailed comparisons. The asymmetric-core collective model of Chi and

    Davidson (Ch 63) and the Hartree-Fock approach of Kelson and Levinson

    23(Ke 64) also fit the first few states of Na and predicted approximate

    locations for some of the higher lying levels. With the exception of

    Litherland and of Rakavy, who admixed only two bands, the above authors

  • 24

    mixed the = 3/2+ , l/2+ , and 5/2+ band and neglected the other three

    band heads in the sd shell on the basis that they were too high in excitation

    to contribute to the low lying spectra. This is partially true, but it has

    since become known that the ground state band mixes strongly with a l/2+

    23hole band located at about 4.4 M e V excitation in Na . The calculation of

    Glockle (G1 64) included the l/2+ hole excitation (Nilsson orbit 6) in

    •J*addition to the 3/2 , 1/2 , and 5/2 bands and obtained a reasonable

    comparison with the experimental data known at that time. But the hole

    excitation band head was incorrectly positioned at 2, 64 MeV, for which

    state the parity has since been shown to be negative.

    The work of Howard et al. (Ho 65) was the first to compare dynamic

    21 21properties for the 3/2, 5/2, and 7/2 band members of Ne , Na , and

    23Na . Considering that Howard completely neglected band mixing, good

    agreement was obtained for the few comparisons made.

    23Aware of the need for additional experimental information on Na ,

    Poletti and Start (Po 66) measured mixing and branching ratios and

    rigorously limited spin assignments for levels up to 2. 98 M e V excitation

    23in Na . Poor experimental statistics and generally weak correlations

    precluded any new or unique spin assignments. Experimental studies have

    also been reported on the J=-| states at (2.39, 2. 64) and 4. 43 M e V (Pe 66)

    and (Me 64), respectively , and on the 2.98 M e V state (Ra 66). Earlier,

    branching ratios and approximate spin assignments were made to some

    levels up to 4. 78 M e V through study of resonance proton capture on

  • 25

    calculations with Coriolis coupling between the four lowest lying bands,

    (using as parameters the band head energy, different moment of inertia

    for each band, deformation, and a generalized spin-orbit coupling constant,

    23for levels below 5. 0 M e V in Na ) were performed by El-Batanoni and

    Kresnon (Ba 67). Also, calculations by Malik and Scholz (Ma 67) mixing

    in all siz bands in the sd shell with a single moment of inertia and the

    23deformation as parameters, were done for levels up to 8. 0 M e V in Na .

    In both calculations the overall fit was good, but again both groups of

    authors were led astray through fitting low lying assumed positive parity

    states that have since been shown to have negative parity. A n important

    difference between the above two calculations is that Malik and Scholz

    calculated band head energies and used the same moment of inertia for

    each band, which reduced considerably the number of parameters used

    in fitting the data. It is also interesting to note that the latter calculation

    predicts the ll/2+ and 13/2+ ground state band members at excitations

    between 5.0 and 7.0 MeV, which is the approximate position predicted by

    the rotor model as well.

    Additional information determined from g a m m a - g a m m a angular

    correlations was reported by Maier (Ma68a); particularly defini-

    “I*tive 7/2 and 9/2 assignments identified the second and third ground state

    23band members of Na . Branching ratio and lifetime information was also

    22Ne (Ar 62, Br 62 ).With the additional experim ental inform ation, new co llective model

  • 26

    In addition to the ground state rotational band and the higher lying

    positive parity states, another series of levels of current interest are the

    negative parity states, believed to be hole excitations generated by

    promoting a particle from orbit 4 to orbit 7. Since the beginning of this

    work, a few negative parity states have definitely been established.

    Reflecting the absence of other low lying negative parity bands, this

    77 _K =1/2 band should exhibit pure rotational behavior, the degree of which

    we have studied herein.

    During the course of this experiment other theoretical and experi

    mental information was reported, but will be discussed later together with

    the results of our current work. A s u m m a r y of the experimental informa-

    23 21tion on Na and Na at the outset of the present measurements is shown

    in the energy level diagram in Fig. 7.

    E. Rotational Structure of Odd Count £ = 1 1 Nuclei

    1. Rotor behavior

    In odd-even nuclei the single particle structure is determined

    as is evident from the Nilsson energy level diagram in Fig. 6, by promoting

    the last odd nucleon into various unoccupied orbits creating single particle

    excitations. Hole excitations m a y be generated by promoting a particle

    from a lower occupied orbit, e. g. (#4), to a higher partially occupied one,

    e. g. (#7). Both types of excitations have been found experimentally in the

    £ = 11 nuclei. In these nuclei, where the number of odd count nucleons

    obtained on som e of the other lev e ls in Na .

  • 6.311 ----------------------------------------------- 1 / 2 *

    Fig. 7

  • 27

    is the same, and under the assumption that the nuclear structure is -

    determined by the last odd nucleon, the sequence of orbits available for

    occupation by the excited single nucleon are identical and, therefore, the

    spectra of nuclei in this scheme should be very similar. As an example,

    excitation spectra of four of the £ = 11 nuclei are shown in Fig. 8 illustra

    ting the 3/2* ground state rotational bands. Other similarities exist in

    these nuclei but are omitted for purposes of clarification. In each nucleus,

    it should be noted that the ground state has the same spin and parity

    followed by a series of rotational levels. This is by no means a trivial

    example; as was noted earlier, in the case of two of the neutron rich

    19 25£ = 11 nuclei, O and Na , ground state spins are not even predicted by

    the strong coupling collective model and the excitation spectra of these

    nuclei possess no obvious rotational structure.

    It is of interest to examine the excitation level sequence more closely.

    21The excitation of the members of the ground state rotational bands of Ne

    21and Na are approximately linearly dependent upon J(J+1), up to the recently

    , + 21 , + 21 established 11/2 m e m b e r in Ne (Ro 69) and the 9/2 members in Na

    21(Pr 69). Higher levels in Na have not been heretofore identified and a

    . + 21possible 13/2 state in Ne is under study (Ro 69a) with excitation energy

    consistent with the J(J+1) rule. The members of the corresponding

    23 +bands in Na w e r e previously known up to the 9/2 m e m b e r

    + +and new measurements, presented herein, identify the 11/2 and 13/2

    members substantiating the systematics suggested by the low lying band

  • EXCITATION

    ENERGY

    (MeV)

    V

    6.450-

    4.431-

    *

  • 28

    members. A plot of excitation energy versus J(J+1) was shown earlier in

    21 23Fig. 3 for Ne and Na illustrating basic structural differences in the

    rotational bands.

    23In Na the levels show oscillatory systematic departures from a

    pure rotor spectrum implying the existence of rotational perturbations,

    21in contrast to the almost pure rotor behavior in Ne . These differences

    provide evidence for rotational anomalies unaccounted for in previous

    collective treatments of these nuclei. The little experimental information

    23 21available on the corresponding mirror nuclei M g and Na confirms the

    above systematics and, therefore, the differences are not an accidental

    23peculiarity of Na itself. Additional evidence supporting this type of

    159rotational behavior has been found in Tb (Gr 67). Here the level

    TT +sequence in the K =3/2 ground state band oscillates in much the same

    23manner as in Na , but the departures from pure rotor behavior are much

    smaller.

    A possible collective mechanism capable of producing the observed

    23level ordering in Na is Coriolis band mixing. Strong Coriolis coupling

    1T + +between a K =3/2 ground state band and a higher lying 1/2 band,

    having a large decoupling parameter producing level inversion in the 1/2

    band itself, could account for the observed effect.

    rr +A higher order effect that could be unusually large in a K =3/2

    band is third^order Coriolis decoupling in the K = 3/2 band itself, similar

    to the decoupling in the K = 1/2 band. Such mechanisms were suggested

  • 2 9

    to account for the results in Tb and are discussed in more detail in

    Section I-F. Both mechanisms are possible explanations but neither

    23 21within the model framework favor Na over Ne .

    F r o m a microscopic point of view, and perhaps more realistically,

    21 23the difference between N e and N a is that the latter has an additional

    7T *1*proton and a neutron in the K = 3/2 orbit. It might be expected that the

    23two neutrons in the K = 3/2 orbit in Na are inertly paired and are

    effectively incorporated in the core leaving the odd proton to generate

    single particle excitations. If residual interactions between the extra-

    20core particles are to be considered, all three nucleons outside of Ne

    23(in the case of N a one proton and two neutrons) would have to be treated,

    which is beyond the scope of contemporary strong coupling models. Up to

    20three neutrons outside a close core of Ne has been considered and such

    approaches have been applied to the neon isotopes with favorable success

    (Cr 69). Also odd-odd nuclei (i. e. one proton and one neutron outside an

    inert core) have been treated including complete Coriolis coupling with

    proper account of isobaric spin (Wa 69). In any case, multiple nucleonic

    excitations in an unfilled subshell outside a closed core are not considered

    in the spirit of the approach taken herein.

    2. Nuclear Rigidity

    Continuing the spirit of the simple rotor model, states of

    high spin should be generated by successive rotations of the nuclear core.

    Locations of the states are determined from the equation

  • 30

    E = ft2/2l J(J+l)

    in the absence of any departure from rigidity. Searching for states of

    high angular m o m e n t u m in light nuclei, where the SU and shell modelsOpred'ct finite limits on the magnitude of the angular m o m e n t u m quantum

    number terminating a rotational band will have interesting consequences.

    In particular, a value exceeding the cutoff would certainly question the

    detailed validity of the shell or, more particularly, the SUQ model to

    23nuclei in this region. A plot of excitation energies versus J(J+1) for Na ,

    up to an extrapolated spin of 17/2 , is shown in Fig. 9. F r o m an empirical fit to the data l A r. 97> found; these almost rigid body values, typical

    of nuclei near mass number 23 are in marked contrast to typical rare

    earth values of l / Y g “ 9- 3- Systematic application of the Coriolis

    coupling model to sd shell nuclei predicted similar results as shown in

    Fig. 10 (Hi 69). Positive deformations have been measured and determined

    from best fits of the data for the nuclei considered herein and, together

    with rigid body moments of inertia, these imply rigid, well-deformed

    prolate nuclei, capable of maintaining rigid deformations up to large values

    of angular m o m e n t u m without significant centrifugal stretching.

    The high spin states, as apparent in the J(J+1) plot, lie at high

    excitation energies exceeding thresholds for particle emission. However,

    cascade de-excitation by electromagnetic g a m m a decay might well remain

    as favored over particle emission in view of the large angular m o m e n t u m

    which would necessarily be carried by the emitted particle. These states

  • EXCI

    TATI

    ON

    ENER

    GY

    EXCITATION ENERGY VERSUS J(J+I)

  • M A S S N U M B E R

    F ig. 10

  • 31

    radiation to and from the lower band members. F r o m the existing

    systematics of the rotational levels and the apparent rigid deformations

    21 23of Ne and Na , it is probable that little centrifugal stretching occurs

    and that a relatively constant moment of inertia is maintained. Therefore,

    levels of excitation may be expected to follow the J(J+1) rule up to large

    angular m o m e n t u m quantum numbers exceeding the largest presently

    measured value of 13/2 ft in light, odd-A, sd shell nuclei.

    F. Rotational Perturbations

    The static properties, and enhancements of certain dynamic

    properties, of the low-lying states of many nuclear species, particularly

    the rare earth nuclei, have been reasonably well accounted for by the simple

    rotor model. Although not quite as successfully, the model has been used

    to interpret properties of the low lying levels of light sd shell nuclei,

    particularly in the first half of the shell.

    In both regions of the periodic table particular nuclei clearly depart

    from rotor behavior without obvious physical reason. These discrepancies

    m a y be explained,on occasion, by adding higher order corrections to the

    rotor Hamiltonian or by treating the existing terms in the Hamiltonian to

    higher order perturbation theory, in effect approximately diagonalizing

    the Hamiltonian. Perturbation treatments in lowest order usually suffice,

    especially in light of the increased computational difficulty in exact

    diagonalization of the total Hamiltonian. Because the exact diagonalization

    may therefore be identified from the ch aracteristics of the cascading

    *6

  • 32

    is done in a truncated space of basis wave functions, this approach is, in

    any case, only reliable for the first few lowest states in the energy

    spectrum.

    In cases where a larger range of states in a rotational band,

    including ones of high excitation energy, are of interest, a perturbation

    treatment is frequently more useful. Here, by exploiting the symmetry

    of the perturbing Hamiltonian, and inspecting the matrix elements in the

    perturbation expansion, it is frequently possible to identify which terms

    give significant corrections to the energy eigenvalues. The calculational

    advantages in applying perturbation theory to the rotor model will be

    demonstrated herein. W e consider the effect of various rotational pertur

    bations on the energy eigenvalues determined from an unperturbed rotor

    model using strong coupling model wave functions.

    1. Nonconstant moment of inertia

    It was noted earlier that if the rotational motion was not

    sufficiently slower than the vibrational motion the adiabatic approximation

    was invalid and that rotation-vibration interaction terms must then be

    incorporated into the total Hamiltonian. The first order correction to the

    Hamiltonian for this interaction is a term of the form (Wo 67, Na 65)

    Hr o t-v ib = -B'J»2'J+1>2where the numerical sign of B has been explicitly written. Such a term

    is well known from the simplest molecular physics studies involving an

    angular m o m e n t u m expansion of the rotational energies (Wo 67). The

  • 33

    Hamiltonian used to fit the early data for M g (Li 58) included this term,

    for example, and its inclusion together with higher order members of the

    angular m o m e n t u m expansion has been most clearly demonstrated in the

    case of heavier nuclei.

    The coefficient B has been calculated by Hamamato (Ha 69) using

    the cranking model formula (In 54) with a Nilsson model Hamiltonian

    including a pairing interaction. The magnitude and sign of B, thus

    obtained, agreed fairly well with data taken for heavy nuclei. By casting

    the above equation in a slightly different form it is possible to interpret

    the correction factor as an apparent increase in the moment of inertia.

    W e m a y write

    H = ft2/2I * J(J+l)

    whereI ' = I / ( 1 - B / a (J)(J+i))

    As J increases the effective moment of inertia increases, which

    physically corresponds to a stretching of the nucleus as it undergoes

    successively faster rotation. Recently, this idea has been more fully

    exploited, resuting in two very interesting, simple, semiclassical

    approaches that have been remarkably successful in accounting systematically

    for collective properties of many heavy, even-A nuclei.

    One is a centrifugal stretching of a classical rotator (So 68) and

    the other is the variable moment of inertia model (VMI) of Mariscotti

    et al. (Ma 68). These models warrant attention in view of their mathema

    tical simplicity and especially in light of their success over a broad range

    25

  • 34

    of nuclei. No doubt that the moment of inertia is not a constant of the

    motion and that any reasonable collective model should include this effect

    in some form or another. However, to employ the centrifugal stretching

    models, a broad range of nuclei with similar rotational properties must

    be kr.own in order to obtain reliable fitting parameters averaged over many

    nuclei. In the mass 21 and 23 region the onset and deterioration of

    rotational behavior is so brief and abrupt that no such averaged fitting

    parameters can be determined.

    In addition both models are designed to apply to even A nuclei

    rather than to odd A nuclei, which are of particular interest in this work.

    2. Higher order Coriolis perturbations

    In light, odd-A nuclei, departure from rotor behavior is

    usually attributed to Coriolis band mixing, where the band heads are

    intrinsic, single-particle states. In heavy deformed nuclei the band heads

    include beta and g a m m a vibrations on the nuclear surface as well as

    single particle excitations. No analogous vibrations have been found as

    yet in light odd A nuclei. We, therefore, confine our attention to rotational

    perturbations generated by the interactions between the orbiting odd

    particle and the core, of which the most c o m m o n form is the Coriolis

    interaction.

    A systematic departure from pure rotor behavior similar to that

    23 +illustrated earlier in Na , was found in the K 7T= 3/2 ground state band

    159of Tb (Gr 63, Bi 66). Although the deviations were much smaller, they

  • 35

    persisted up to the highest then known band m e m b e r (J = 23/2). It was

    discovered that the energy levels of the 3/2 band could be fitted with an

    expansion of the form

    where A,B, and C are parameters determined by fitting the data (Gr 63).

    The exact physical origin of. the last term, which we shall refer to as

    third order Coriolis decoupling, is unclear in that the angular m o m e n t u m

    dependence of such a term can be calculated by starting with different

    forms of the Hamiltonian. To obtain a better understanding of its possible

    origins, we consider it in more detail.

    Treating the Coriolis interaction

    as a perturbation and using the unperturbed strong coupling model wave

    functions

    the corrections to the energy eigenvalues may be conveniently calculated

    corrections are calculated in the appendices given herein.

    Since the basis functions form a complete orthogonal set and the

    E(J) = A(J)(J+1) + B J2(J+1)2 + C(-l)J+^(J4)(J+|)(J+3/2)

    H ' = -2A (J+j_ + J-j+)

    up to third order in a perturbation expansion of the usual form (Sc 68)

    m m m m m

    where is the unperturbed energy of the mth state and the additional

  • 36

    Coriolis perturbation has no diagonal contribution in a K = 3/2 band,

    there is no contribution in first order (i. e. = 0).

    It is shown in Appendix I that corrections in second order can be

    written in the form

    E (2) = A i+A 2 (J)(J+3)

    and are equivalent to a renormalization of the moment of inertia and band

    head energy. Such corrections are obviously already included in the simple

    rotor model when the coefficient of J (J+l) is treated as a parameter in

    fitting the data.

    The first nontrivial correction appears in third order and the cal

    culation in Appendix II yields a term of the form

    e(3) = ("1)J+3/2

  • 37

    another approach leading to a term of the same angular momentu m

    dependence, but without inclusion of band mixing, is to effectively expand

    —*-2the Hamiltonian in a power-series in R . Recall that the rigid rotor part

    of the Hamiltonian was written as

    W e begin by phenomenologically assuming that l / l m a y be written as a

    -*2slowly varying function f(aR ) where a is a small constant (Mi 64).

    Justification for such a function is by no means rigorously based. Since

    the Hamiltonian must be a scalar and the effects of centrifugal core

    distortion are independent of the axis of rotation and in analogy with the

    treatment of molecular rotation (Wo 67), the simplest nontrivial non

    vector ial fuction that can be expanded in a power series is a function of

    2the form f(aR ). Substituting

    ~=f(aR2)

    2 2 in the above Hamiltonian and expanding f(aR ) in a power series in aR

    f(aR2) = l / l (B + B (aR2) + B (aR2)2 + . . .) ,O O i / 2the rotor Hamiltonian m a y then be written in the form

    H = *- E A (R2)w ,2Iq i/=0 uwhere I is the moment of inertia at rest and A are constants determined o vby the internal motion of the nucleus.

    It should be noted that this is not the most general angular m o m e n t u m

  • 38

    expansion (Mi 64), but it suffices to illustrate how higher order diagonal

    contributions m a y be included in the rotor model. However, assuming

    that centrifugal distortions preserve axial symmetry and R remainsOzero, the above form is indeed correct within the framework of the rotor

    model. A n expansion in powers of J ± systematically including higher order

    Coriolis perturbations is given by Bohr and Mottelson (Bo 69).

    Recalling that S = J-j and using the strong coupling rotor model

    wave functions, the calculation of all diagonal contributions or first order

    2 3corrections to the energy, up to the (R ) term, is shown in Appendix IV.

    The result is an expression for the energy written as3

    E = AJ(J+l)+B J2 (J+l)2+C [ J3(J+l)3-8(J-^(J+|)(J+|)(-l)J+2"a3/2]

    where *s definec* as K = 3/2 third order decoupling parameter

    r i J-3/2ln ,2w _iwiJ

    j

    in complete analogy with the more familiar K = 1/2 decoupling parameter.

    a3/2= £ (“1) lC j3/2 I

  • 39

    identical, the Hamiltonian expansion in power of R reflects vastly

    different physical behavior than does the strong coupling rotor model with

    Coriolis interaction. In the former the nucleus is imagined to undergo

    complicated rotations and vibrations, neither motion being spelled out

    explicitly, while in the latter the nuclear motion is predominantly

    rotational with strong Coriolis coupling between the odd particle and the

    core. Distinguishing between these two kinds of motion is virtually

    impossible from energy level consideration alone, primarily because of

    the similarity of their angular m o m e n t u m dependence.

    4. Wave function admixtures

    Calculations have only been presented to show the effects

    of perturbations on the rotational levels themselves, but generally speaking,

    the corresponding wave functions will have additional components resulting

    from these rotational interactions. A n exception to this generality is the

    angular m o m e n t u m expansion calculation where only diagonal contributions

    to the energy were considered. Here, the strong coupling rotor model

    wave function remains unchanged. In the explicit band mixing calcula

    tions, K no longer remained a good quantum number introducing con

    figurational mixing into the wave functions. Although the eigenvalue

    dependence on the angular m o m e n t u m is the same up to third order, the

    eigenfunctions corresponding to the Hamiltonians are different. These

    unmixed and admixed wave functions m ay all be used to calculate transi-

    2

  • 40

    tion strengths and by comparing the results of the calculation with

    experiment the form of the Hamiltonian that best describes the nuclear

    motion may be determined.

    In transitions that are predominantly forbidden or hindered by the

    Alaga asymptotic selection rules (Al 57, W a 59), the transition probabilities

    obviously may become more sensitive to the wave function admixtures.

    In certain instances the smaller admixed portion of the wave function may

    provide the dominant contribution to the transition. Examples are

    electric dipole interband transitions between the excited K 77 = 1/2 and the

    — + 23K = 3/2 ground state rotational band in Na . Here it is essential to

    include the wave function admixtures to obtain any agreement with experi

    ment as will be demonstrated herein.

    A more general approach to the problem has been discussed by

    Mottelson (Bo 69, M o 67, Mi 66, Gr 64) where the El transition matrix element

    is written effectively as an expansion in powers of angular m o m entum

    similar to the above mentioned energy expansion. In particular the El

    transition probability was written as

    B(E1) = M 1 + [I.(I.+1) -If(If+l)] M 2

    where M is the usual electric dipole contribution and the second term isi ■*-the lowest order correction from the angular m omentum expansion. This

    approach was found to provide agreement with the available experimental

    data (Mo 67). The disadvantage of this particular form of expression is

  • 41

    that it is independent of the particular interaction and can not be used to"

    select the perturbation mechanism. The power expansion does provide us

    with the lowest order I dependence and at least we know the analytic form

    that should be approximated by any explicit calculation.

    G. Model Comparison Using Electromagnetic Properties

    The quality of a model calculation for sd shell nuclei has been

    judged in most cases by fitting excitation energies and angular momentum

    quantum numbers, and in certain cases spectroscopic factors. This crude

    test of a model is sufficient when differentiating between the asymptotic

    extremes of the shell and collective models. In most cases nuclei show

    intermediate behavior and on the basis of the above comparisons the

    models may be virtually indistinguishable. A more rigorous test of the

    model wave function, must then be obtained. Such a test involves

    comparison of the matrix elements of the dynamic observables in addition

    to the static ones. More specifically, herein we examine the electro

    magnetic transition rates, g a m m a de-excitation branching ratios, multi

    pole mixing ratios, etc. In particular we concentrate on the electro

    magnetic properties of the nucleus in these comparisons. These are

    experimentally and theoretically the most reliable in view of our relatively

    fundamental and extensive knowledge of the electromagnetic interactions

    in nuclei. The fact that this interaction is weak in comparison to the strong

    interactions of the nuclear constituents permits the use of lowest order

    perturbation theory (e. g. Fermi’s Golden Rule II) to calculate transition

  • 42

    probabilities. Even in the case where higher order effects are of

    interest, it is an ardous but straight forward computational task to

    include them.

    It was the inherent inability of the shell model to correctly predict

    the large quadrupole moments of nuclei and the enhanced E2 transition

    probabilities that motivated the development of the collective model (Bo 52,

    Bo 53), These enhanced properties have since become the signature of

    nuclear collective behavior, and are most pronounced in the present work.

    H. Experimental Method

    The experimental techniques for measuring angular m o m entum and

    nuclear dynamic electromagnetic properties are standard and the objec

    tivity of data interpretation combines to lead to a very reliable source of

    spectroscopic information. In addition a rigorous statistical analysis of

    errors can be performed on such measurements and can be used in dis

    criminating against unsatisfactory fitting parameters or models on the

    basis of well established and precisely defined confidence levels.

    Incorporating these desired features is the standard Method II

    particle-gamma angular correlation technique first suggested by

    Litherland and Ferguson (Li 61).- In the experiment reported herein, the

    method was used in the form described by Poletti and Warburton (Po 65).

    A derivation of the angular distribution formula (Ro 67) used herein is

    given in Appendix V.

  • 43

    1 . G a m m a r a y a n g u l a r d i s t r i b u t i o n f r o m a l i g n e d n u c l e i :

    O u r e x p e r i m e n t s b a s i c a l l y c o n s i s t o f m e a s u r i n g a n a n g u l a r

    d i s t r i b u t i o n o f g a m m a r a y s e m i t t e d f r o m p r e f e r e n t i a l l y a l i g n e d n u c l e a r

    s t a t e . T h e r e s i d u a l n u c l e u s i n t h e s e l e c t e d n u c l e a r r e a c t i o n i s a l i g n e d

    w i t h r e s p e c t t o t h e p r o j e c t i l e b e a m a x i s ; t h i s a l i g n m e n t i s a c h i e v e d b y

    c o n s t r a i n i n g t h e e f f e c t i v e p o p u l a t i o n o f m a g n e t i c s u b s t a t e s t h r o u g h t h e

    d e t e c t i o n o f g a m m a r a y s i n c o i n c i d e n c e w i t h t h e l i g h t o u t g o i n g r e a c t i o n

    p r o d u c t i n a n a n n u l a r c o u n t e r a x i a l l y p o s i t i o n e d v e r y c l o s e t o 1 8 0 d e g r e e s .

    T h e a x i a l g e o m e t r y d e f i n e d b y t h i s c o u n t e r p e r m i t s p o p u l a t i o n o f t h o s e

    m a g n e t i c s u b s t a t e s w h o s e m a g n e t i c q u a n t u m n u m b e r i s l e s s t h a n o r e q u a l

    t o t h e s u m o f t h e s p i n s o f t h e t a r g e t n u c l e u s , t h e i n c o m i n g , a n d t h e o u t

    g o i n g p a r t i c l e s ; a s i m p l e p r o o f o f t h i s c o n d i t i o n i s g i v e n i n A p p e n d i x V I .

    T h i s t e c h n i q u e m i n i m i z e s t h e n u m b e r o f f i t t i n g p a r a m e t e r s u s e d i n t h e

    a n a l y s i s o f t h e d a t a a n d i s e s s e n t i a l i n m a k i n g u n i q u e s p i n a s s i g n m e n t s .

    M o s t i m p o r t a n t , h o w e v e r , i s t h e b a s i c f a c t t h a t i t m a k e s t o t a l l y u n n e c e s

    s a r y a n y k n o w l e d g e o f t h e m e c h a n i c s o r i n t e r m e d i a t e s t a t e s o f t h e p o p u l a

    t i n g r e a c t i o n a s i s e s s e n t i a l i n , f o r e x a m p l e , t h e m o r e f a m i l i a r a n a l y s i s

    o f a n g u l a r c o r r e l a t i o n s f o l l o w i n g r e s o n a n c e r e a c t i o n s .

    I f t h e a n g u l a r m o m e n t u m q u a n t u m n u m b e r o f t h e l e v e l o f i n t e r e s t

    i n t h i s a p p r o a c h i s n o t u n i q u e l y a s s i g n e d , i t i s a t l e a s t r i g o r o u s l y l i m i t e d

    t o a f e w p o s s i b i l i t i e s . A t t h e s a m e t i m e t h e e l e c t r o m a g n e t i c m u l t i p o l e

    m i x i n g r a t i o i s d e t e r m i n e d a s a f i t t i n g p a r a m e t e r f r o m t h e m e a s u r e d

  • 44

    a n g u l a r d i s t r i b u t i o n o f g a m m a r a y s a n d b y s u m m i n g t h e g a m m a r a y y i e l d

    f r o m a g i v e n s t a t e o v e r a l l a n g l e s , t h e b r a n c h i n g r a t i o o f t h e s t a t e m a y

    b e d e t e r m i n e d .

    C o m p l i m e n t a r y t o s u c h a n g u l a r c o r r e l a t i o n d a t a a r e l i f e t i m e i n f o r

    m a t i o n ( i . e . a b s o l u t e t r a n a t i c n m a t r i x e l e m e n t s ) a n d R v a l u e a s s i g n m e n t s

    f r o m s i n g l e p a r t i c l e t r a n s f e r d a t a y i e l d i n g u n i q u e p a r i t y a s s i g n m e n t s a n d

    a g a i n a f e w s p i n p o s s i b i l i t i e s . B y c o m b i n i n g t h e s p i n p o s s i b i l i t i e s f r o m

    b o t h s e t s o f d a t a , p a r t i c u l a r l y w h e n , w i t h o n e e x c e p t i o n , t h e s e s e t s a r e

    m u t u a l l y e x c l u s i v e , a r i g o r o u s a s s i g n m e n t m a y b e m a d e .

    N u c l e a r l i f e t i m e i n f o r m a t i o n m a y b e u s e d t o d e t e r m i n e t h e a b s o l u t e

    t r a n s i t i o n m a t r i x e l e m e n t s o f a g a m m a r a y t r a n s i t i o n w h e n c o m b i n e d w i t h

    t h e m i x i n g r a t i o o f t h e t r a n s i t i o n . I n p a r t i c u l a r , i f t h e e l e c t r i c s t r e n g t h

    2e x c e e d s t h e W e i s s k o p f e s t i m a t e b y Z , t h e c o r r e s p o n d i n g s p i n m a y

    r e a s o n a b l y b e r e j e c t e d . W e m a y t h e n e x t r a c t t h e r e d u c e d t r a n s i t i o n

    p r o b a b i l i t y f o r t h e a c c e p t e d s p i n a n d w e h a v e a n a d d i t i o n a l e l e c t r o m a g n e t i c

    q u a n t i t y t o c o m p a r e w i t h a n u c l e a r m o d e l .

    2 . R e a c t i o n s

    I n t h e w o r k d i s c u s s e d h e r e i n , M e t h o d I I c o r r e l a t i o n s t u d i e s

    2 3 2 1 2 3 2 3 2 6w e r e c a r r i e d o u t o n N a a n d N a t h r o u g h t h e N a ( a , o : V ) ^ a » ( P . c v y )

    2 3 2 4 2 3 2 4 2 1N a , M g ( t . a y J N a , a n d M g ( p , o » y ) N a r e a c t i o n s , r e s p e c t i v e l y . T h e

    M P t a n d e m V a n d e G r a a f f a c c e l e r a t o r i n t h e W r i g h t N u c l e a r S t r u c t u r e

  • 45

    L a b o r a t o r y a t Y a l e U n i v e r s i t y p r o v i d e d b o t h t h e a l p h a - p a r t i c l e a n d t h e

    p r o t o n b e a m s w h i l e t h e 3 M V V a n d e G r a a f f a c c e l e r a t o r a t t h e B r o o k h a v e n

    N a t i o n a l L a b o r a t o r y p r o v i d e d t h e t r i t o n b e a m .

    3 . B a c k g r o u n d r a d i a t i o n d i f f i c u l t i e s

    A t Y a l e , w h e r e t h e p r o t o n i n d u c e d r e a c t i o n s w e r e c a r r i e d

    o u t a n d f r o m w h i c h t h e b u l k o f t h e e x p e r i m e n t a l d a t a w a s o b t a i n e d , h i g h

    e n e r g y p r o t o n b e a m s o f 1 4 . 2 5 M e V a n d 1 7 . 5 0 M e V w e r e r e q u i r e d i n o r d e r

    t o c l e a r l y d i s c e r n t h e h i g h e r s t a t e s o f e x c i t a t i o n . T h e s e h i g h b o m b a r d

    m e n t e n e r g i e s , n o t n o r m a l l y u s e d i n M e t h o d I I c o r r e l a t i o n s t u d i e s , p r e

    s e n t e d s o m e s e v e r e e x p e r i m e n t a l d i f f i c u l t i e s t h a t h a d t o b e s u r m o u n t e d

    b e f o r e t h e e x p e r i m e n t s w e r e s u c c e s s f u l l y c o n d u c t e d . T h e m o s t c h a l l e n g

    i n g w a s t h e r e d u c t i o n o f t h e i n t e n s e n e u t r o n a n d g a m m a r a y b a c k g r o u n d

    r a d i a t i o n g e n e r a t e d b y a d d i t i o n a l o p e n r e a c t i o n c h a n n e l s a t t h e h i g h e r

    p r o t o n b o m b a r d m e n t e n e r g i e s . T o m i n i m i z e t h e r a d i a t i o n d i f f i c u l t i e s

    t h e b e a m t r a n s p o r t s y s t e m w a s d e s i g n e d t o f o c u s t h e b e a m t h r o u g h a n

    a n n u l a r c o u n t e r w i t h o u t s t r i k i n g t h e s h i e l d i n g m a t e r i a l o r , f o r t h a t

    m a t t e r , a n y m a t e r i a l i n t h e v i c i n i t y o f t h e r a d i a t i o n d e t e c t o r s ( p a r t i c l e o r

    g a m m a r a y ) o r t a r g e t . M o r e s p e c i f i c b e a m t r a n s m i s s i o n a n d f o c u s s i n g

    c o n d i t i o n s a n d o t h e r p r o b l e m s a r e d i s c u s s e d i n t h e a p p r o p r i a t e s e c t i o n s

    o f s u c c e e d i n g c h a p t e r s .

  • 46

    T h e w o r k p r e s e n t e d h e r e i n f o c u s s e s o n t h e m a s s 2 1 a n d 2 3 r e g i o n

    w h i c h h a s l o n g b e e n r e c o g n i z e d a s o n e d e m o n s t r a t i n g m a r k e d c o l l e c t i v e

    2 1 2 3b e h a v i o r . A d e t a i l e d s t u d y o f t w o s e l e c t e d n u c l e i , N a a n d N a h a s

    b e e n u n d e r t a k e n u t i l i z i n g f c e . a ' y ) , ( P . a y ) . a n d ( t , a y ) r e a c t i o n s o n i

    a p p r o p r i a t e t a r g e t s . N o w s t a n d a r d c o l i n e a r c o r r e l a t i o n g e o m e t r i e s h a v e

    b e e n u s e d t o s t u d y g a m m a r a d i a t i o n f r o m a l i g n e d r e s i d u a l s t a t e s a n d a n

    o n - l i n e c o m p u t e r s y s t e m h a s b e e n u t i l i z e d i n d a t a a c q u i s i t i o n a n d r e d u c t i o n .

    P a r t i c u l a r i n t e r e s t h a s b e e n f o c u s s e d o n t h e K ^ = 3 / 2 + g r o u n d

    21s t a t e r o t a t i o n a l b a n d s . I n N a , c l o s e a g r e e m e n t o f t h e o b s e r v e d l e v e l

    e x c i t a t i o n w i t h t h o s e e x p e c t e d i n a p u r e r o t o r s p e c t r u m h a s b e e n f o u n d .

    2 3W h e r e a s i n t h e s u p p o s e d l y d i r e c t l y c o m p a r a b l e s i t u a t i o n i n N a , a l s o a

    £ = 1 1 n u c l e u s , a n d t h e r e f o r e e q u i v a l e n t o n t h e b a s i s o f a N i l s s o n m o d e l ,

    s t r i k i n g o s c i l l a t o r y d e v i a t i o n s f r o m r o t o r p r e d i c t i o n s a r e o b s e r v e d .

    T h i s s u g g e s t s a C o r i o l i s b a s e d e x p l a n a t i o n b u t s u c h i s n o t y e t a v a i l a b l e i n

    s a t i s f a c t o r y f a s h i o n .

    C o m p l i c a t i n g t h e s i t u a t i o n i s t h e f a c t t h a t i n b o t h n u c l e i , t h e m o m e n t s

    o f i n e r t i a a r e i n e x c e s s o f 9 0 % o f t h e r i g i d b o d y v a l u e s a n d t h e i n t r i n s i c

    e l e c t r i c q u a d r u p o l e m o m e n t s o f t h e m e m b e r s o f t h e r o t a t i o n a l b a n d s a p p e a r

    t o r e m a i n r e l a t i v e l y c o n s t a n t u p t o t h e h i g h e s t e x c i t a t i o n s s t u d i e d ( J = 1 3 / 2 ) .

    T h e s e d a t a s u g g e s t t h a t t h e s e n u c l e i m a y w e l l b e t h e m o s t r i g i d i n t h e

    I . Sum m ary

  • 47

    p e r i o d i c t a b l e , b u t a l s o t h e r e a r e a s p e c t s o f c o l l e c t i v i t y e v e n i n t h e s e

    r e l a t i v e l y s i m p l e n u c l e i , w h i c h a r e n o t a d e q u a t e l y u n d e r s t o o d .

    !

  • 48

    I I . A P P A R A T U S

    T h e u s e o f s p i n z e r o a n d s p i n o n e h a l f p a r t i c l e s a s n u c l e a r

    r e a c t i o n p r o b e s i n M e t h o d I I c o r r e l a t i o n s t u d i e s o n s p i n 0 t a r g e t s

    r e s t r i c t s m a g n e t i c s u b s t a t e p o p u


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