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28 Roark Flat Plates

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ROARK FLAT PLATES EXHAUST STACK ENGINEERING with the SPREADSHEET Copyright 2006 American Society of Civil Engineers A B C D E F G H I J K L 2 FLAT CIRCULAR PLATES / CONSTANT THICKNESS Roark, 5th Edition Table 24 pg 334 a 2.400 in radius to outer edge Check plate bending with several models b 0.880 in radius to inner edge from Roark and Young page 334 1.600 in radius to location of w APPROXIMATE RADIUS OF BOLT HEAD P 42.90 k For allowable P allowed working calculated in the Bolt Group Pullout template trib length 10.05 in ALONG EDGE OF WASHER a 2.400 w 4267 lb/in point load / circumference line load ro 1.600 q_uniform 2371 uniformly distributed load r_ 1.00 in radial location of evaluated quantity b 0.880 t 1.000 in thickness of plate v 0.285 unit poisson ratio E 29000 ksi Young's modulus of elasticity 1.600 CONSTANTS........................... G_3' -1.67 C_1' 0.24 G_3 0.0000 0.42 G_6' 0.62 C_1 0.658320 unit G_6 0.0000 G_9' -0.58 C_2' 0.40 G_9 0.0000 C_2 0.148945 L_3' 0.59 C_3' 1.14 -0.56 C_3'' -0.87 L_3 0.0050 Figure 28-1 PLAN VIEW OF PLATE C_3 0.024992 L_6' 0.26 C_4 1.210583 L_6 0.0426 C_5 0.432778 L_9' 0.26 0.10 C_6' 1.14 L_9 0.2399 C_6 0.104596 L_11' 1.79 C_7 1.084433 unit L_11'' -4.35 L_11 0.0004 C_8' 0.10 C_8 0.690564 L_14' 0.80 L_14'' -0.72 C_9' 0.64 L_14 0.0051 C_9'' 0.15 C_9 0.293091 L_17' 0.86 L_17'' 1.52 D 2630314 lb-in plate constant L_17 0.0451 29,000 * 1.00^3 / ( 12 * ( 1 - 0.285^2) ) * 1000 lb/k F_1' 0.08 psi F_1 0.13 k = 1000 Lbs. F_2' 0.97 F_2 0.01 F_4' 0.63 F_4 0.72 F_5 0.11 F_6 0.01 F_7 0.12 F_9' 0.08 0.00 F_9 0.07 ro lb/in 2 ro / r lb/in 2 =
Transcript
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ROARK FLAT PLATESEXHAUST STACK

ENGINEERING with the SPREADSHEETCopyright 2006 American Society of Civil Engineers

A B C D E F G H I J K L M

28

FLAT CIRCULAR PLATES / CONSTANT THICKNESS Roark, 5th Edition Table 24 pg 334a 2.400 in radius to outer edge Check plate bending with several modelsb 0.880 in radius to inner edge from Roark and Young page 334

1.600 in radius to location of w

APPROXIMATE RADIUS OF BOLT HEADP 42.90 k For allowable P allowed working calculated in the Bolt Group Pullout templatetrib length 10.05 in ALONG EDGE OF WASHER

a 2.400w 4267 lb/in point load / circumference line load ro 1.600q_uniform 2371 uniformly distributed load

r_ 1.00 in radial location of evaluated quantity b 0.880

t 1.000 in thickness of platev 0.285 unit poisson ratioE 29000 ksi Young's modulus of elasticity

1.600

CONSTANTS........................... G_3' -1.67C_1' 0.24 G_3 0.0000

0.42 G_6' 0.62C_1 0.658320 unit G_6 0.0000

G_9' -0.58C_2' 0.40 G_9 0.0000C_2 0.148945

L_3' 0.59C_3' 1.14 -0.56C_3'' -0.87 L_3 0.0050 Figure 28-1 PLAN VIEW OF PLATE/WASHER C_3 0.024992

L_6' 0.26C_4 1.210583 L_6 0.0426

C_5 0.432778 L_9' 0.260.10

C_6' 1.14 L_9 0.2399C_6 0.104596

L_11' 1.79C_7 1.084433 unit L_11'' -4.35

L_11 0.0004C_8' 0.10C_8 0.690564 L_14' 0.80

L_14'' -0.72C_9' 0.64 L_14 0.0051C_9'' 0.15C_9 0.293091 L_17' 0.86

L_17'' 1.52D 2630314 lb-in plate constant L_17 0.0451

29,000 * 1.00^3 / ( 12 * ( 1 - 0.285^2) ) * 1000 lb/k

F_1' 0.08 psiF_1 0.13 k = 1000 Lbs.F_2' 0.97F_2 0.01F_4' 0.63F_4 0.72

F_5 0.11

F_6 0.01

F_7 0.12

F_9' 0.080.00

F_9 0.07

ro

lb/in2

ro / r

lb/in2 =

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ROARK FLAT PLATESEXHAUST STACK

ENGINEERING with the SPREADSHEETCopyright 2006 American Society of Civil Engineers

A B C D E F G H I J K L M

28

0 logic 1.000 > 1.600 singularity factorr ro

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ROARK FLAT PLATESEXHAUST STACK

ENGINEERING with the SPREADSHEETCopyright 2006 American Society of Civil Engineers

A B C D E F G H I J K L M

28

FLAT CIRCULAR PLATES / CONSTANT THICKNESS -- ContinuedRoark Table 24, Case 2k: Outer edge free, inner edge simply supported… page 342INPUTS FROM ABOVEa 2.400 in radius to outer edgeb 0.880 in radius to inner edge

1.600 in radius to location of w

q_uniform 2371 uniformly distributed load not used in this analysis

t 1.00 in thickness of platev 0.29 unit Poisson ratio 0.88E 29000 ksi Young's modulus of elasticity

2371

0

0 per Roark

0

0

-0.01149 =-q*(a^3)/(D*C7)

0.22204 =(C_9/(2*A*B))*(A^2-RO^2)

-0.00255 radian -0.00255

4310 lb/in shear

( 2,371 /(2 * 0.880 )) * ( 2.400^2 - 1.600^2 ) 2.40

-0.0040 Figure 28-2 PLATE LOADING AND DEFLECTION

0.0006

0.0000

-0.0035 in deflection

Q unit shear lb / inch of circumference

-0.00309 unit applied line moment in-lb / inch of circumference

0.00099 unit radial bending in-lb / inch of circumference

0.00006 unit tangential bending in-lb / inch of radius

-0.00216 radian

r 1.00 in radial location of quantity being evaluated -- input from above

-5231 lb-in/in theta * D * (1 - v^2) /r + v * Mr

-0.00216 * 2,630,314 * (1 - 0.285^2) /1.600 + 0.285 * 0

t 1.0000 in from input aboveS 0.16667

-31

CANTILEVER PLATE COMPARISONq 2371 psiL 1.96 in

M_pl 4554 lb-int_pl 1.00 inS_pl 0.16667

27.32 ksi

ro

lb/in2

yb

Mra

Mrb

Qa

qb'

qb''

qb

Qb

(Q_uniform / (2 * b)) * ( a2 - ro2 )

ya'

ya''

ya'''

ya

qa' Mo

qa'' Mr

qa''' Mt

qa

Mt

in3 1 * t2 / 6

fb k/in2 Mt / S

in3

fb

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ROARK FLAT PLATESEXHAUST STACK

ENGINEERING with the SPREADSHEETCopyright 2006 American Society of Civil Engineers

A B C D E F G H I J K L M

28

Figure 28-3 CANTILEVERED ANCHOR PLATE

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ROARK FLAT PLATESEXHAUST STACK

ENGINEERING with the SPREADSHEETCopyright 2006 American Society of Civil Engineers

A B C D E F G H I J K L M

28

FLAT CIRCULAR PLATES / CONSTANT THICKNESS -- ContinuedRoark Table 24, Case 1a: Outer edge simply supported, inner edge free … page 335

0.1406

0.00 in -4,267 * 2.40^3 / 2,630,314 * 0.1406

lb/in in^3 / lb-intheta_b' 0.22theta_b -0.001

Mrb' 0.00Mrb 0.00

Qb' 0.00Qb 0.00 lb/in

y' 0.00y'' 0.00y''' 0.00y'''' 0.00y 0.00

theta' 0.00theta'' 0.00theta''' 0.00theta'''' 0.00theta -0.001

Figure 28-4 PLATE LOADING Mr' -266.80Mr'' 0.00Mr''' 0.00Mr'''' 0.00Mr -266.80 lb-in

Mt -1576.45 lb-in tangential moment / inch of circumference MOMENT

S provided 0.1666667 1.0000^3 /6

fb -9459-9.5 ksi

Q =B164*b/r_-W*ro/r_*___*_R_RO_theta_a

Qa -2844.89 lb / inch of circumference SHEAR

Figure 28-5 PLATE LOADING

Mt Mt

yb yb

bending in twisting on plate bending in plate / washer

Figure 28-6 PLATE TWISTING Figure 28-7 PLATE BENDING

yb'

yb

in3/in

lb/in2 /in stress in plate

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ROARK FLAT PLATESEXHAUST STACK

ENGINEERING with the SPREADSHEETCopyright 2006 American Society of Civil Engineers

A B C D E F G H I J K L M

28

FLAT CIRCULAR PLATES / CONSTANT THICKNESS -- ContinuedValues from above for Roark Table 24, Case 1a page …. 362a 2.4 in radius to outer edgero 1.6 in radius to location of wq 2371 lb/in^2

t 1 in thickness of platev 0.285 unit poisson ratioE 29000000 psi Young's modulus of elasticity

Roark, Table 24 Case 10a: Outer edge simply supported … page 363 Figure 28-8 PLATE BENDING DIAGRAM

0 per Roark supported edge

0 simply supported edge

L_11 0.000 from aboveL_17 0.045 from above

-0.0005 in

-2,371 * 2.400^4 /(2 * 2,630,314) * ( 0.04514 /(1 + 0.285) - 2 * 0.00044)deflection at center of plate

616 lb-in

S 0.1666667

3698 psi shear force

0.0007 radians q/(8*D*a*(1-v)) * (a^2-ro^2)^2

Qa -1580.50 -q/(2*a)*(a^2-ro^2)L/9,374

Figure 28-9 PLATE SUPPORT Roark Table 24, Case 10b: Outer edge fixed supported … page 363ya 0 per Roark supported edgetheta_a 0 fixed edge

L_11 0.000 from aboveL_14 0.005 from aboveL_17 0.045 from aboveyc 0.000 in -q*a^4/(2*D)*(L_14-2*L_11) deflection at center of plateMc 616.37 lb-in q*a^2*L_17 M at center of plateMra -526.832 lb-in -q/(8*a^2)*(a^2-ro^2)^2 M at fixed edge of plate

L/75,994

S_plate 0.167 in^3 b*t^3/6M 616 lb-infb 4 k/in^2

Figure 28-10 VIEW OF PLATE DEFLECTION

ya

Mra

yc -q * a4 /(2 * D) * (L_17 /(1 + v) - 2 * L_11)

Mc q * a2 * L_17 M at center of plate

in3

fb

qa

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Figure 28-1 PLAN VIEW OF PLATE/WASHER row 40

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not used in this analysis

row 90

-0.00216

row 110

lb / inch of circumference

in-lb / inch of circumference

in-lb / inch of circumference

row 120

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