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Third EUROnu Annual Meeting, RAL 2011
A.WRÓBLEWSKI & B.SZYBIŃSKI
Cracow University of Technology
Assessment of the cooling options for a Superbeam horn
Boundary conditions
How to determine the film coefficient h?
1.Engineering tables2.Simplified relations3.General convection theory (rather complicated approach)
In all above given cases two possibilities considered
1.Natural convection (slow velocity of cooling medium)
2.Forced convection
Engineering tables
Cooling medium Natural convection Forced convection
Gas 5-30 30-500
in Km
W
deg2
Simplified relations (J.P. Holman, Heat transfer)
Horizontal cylinders; convection to air
Laminar104 < Gr · Pr < 109
TurbulentGr · Pr > 109
2/1
27.0
dT
h 2/118.0 Th
degFfthrBtu
In 2
degKmW
674466.55/90.09290304
2928104.0degFfthr
Btu22
degKmW
0.9]m[160.1
degKmW
5.39]m[060.0
deg40
2
2
hd
hd
KT
o
i
Volume [m^3] Energy curr. [W] Energy part. [W]
Front face 0.417046401E-02 1400 757
Inner cond. cylinder 0.396308981E-03 6540 density by Christoph
Inner cond. conic1 0.124743689E-02 2500 1756
Inner cond. cylinder2 0.244735258E-02 1000 1117
Inner cond. conic2 0.126037287E-02 2600 584
Inner cond. cylinder3 0.120818048E-04 density like inn. conductor
357
Exit face 0.384374028E-02 4000 480
Outer cond 0.227386003E-01 1300 3344
ho=1000, he=500, hr=100 , hc=100, hi=10To=293, Te=293 , Tr=293 , Tc=293, Ti=310
ho=1000, he=500, hr=100 , hc=100, hi=10000To=293, Te=293 , Tr=293 , Tc=293, Ti=310
ho=1000, he=500, hr=100 , hc=100, hi=10000To=293, Te=293 , Tr=293 , Tc=293, Ti=310
ho=1000, he=500, hr=100 , hc=1000, hi=10000To=293, Te=293 , Tr=293 , Tc=293, Ti=310
hc: 1001000
ho=1000, he=500, hr=50 , hc=1000, hi=10000To=293, Te=293 , Tr=293 , Tc=293, Ti=310
hr: 10050
ho / To hi / Ti he / Te hr / Tr hc / Tc Current Particle Max. T300 / 350 kA
1 1000293
10310
500293
100293
100293
Yes No 21972879
2 1000293
10000310
500293
100293
100293
Yes No 336350
3 1000293
10000310
500293
100293
100293
Yes Yes 403417
4 1000293
10000310
500293
100293
1000293
Yes Yes 365377
5 1000293
10000310
500293
50293
1000293
Yes Yes 428450
Horn shell with double skin (only in inner part of cylinder )
Horn shell with double skin (only in inner part of cylinder )
Horn shell with double skin (only in inner part of cylinder )
FEM modelling in ANSYS with fatigue calculations
Fatigue analysis – VHCF S-N CurveFatigue analysis – VHCF S-N Curve
841.k
88120
66437.
.numk
%.172
k
knumk