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NSTX

NSTX. Supported by. NSTX Centerstack Upgrade Project Meeting P. Titus/EA Branch February 2 2011. Global Model Update Status P4 Quench Vessel/Bellows Analysis Response Spectra Modal Analysis TF Shear Stress/Influence Coefficients Pedestal Analysis Status. Jan 19 2011 IGES from Mark.

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NSTX

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  1. NSTX Supported by NSTX Centerstack Upgrade Project Meeting P. Titus/EA Branch February 2 2011 Global Model Update Status P4 Quench Vessel/Bellows Analysis Response Spectra Modal Analysis TF Shear Stress/Influence Coefficients Pedestal Analysis Status

  2. Jan 19 2011 IGES from Mark V’s aren’t misaligned 2010 IGES from Mark

  3. Plates are modeled as 1 inch rather than 1.5 r,19,.0254 ! Arch reinforcing plates

  4. The Ring is Segmented? What are the loads from the TF flag/ring Proposed Reinforcement Analyzed Reinforcements

  5. Run #27 Global Model Updates – Inclusion of Pete Rogoff’s Bellows Geometry, ref Calc # NSTXU CALC 133-10-00 -Inclusion of Tile Weights from Art Brooks Calculation n# NSTXU CALC 11-03-00 Mat 11 Mat 8 Cas5.dat Mat 11 r,11,.030/39.37 ! Bellows Thickness /COM MAT,11 Bellows EX,11,200e9 $DENS,11,8.0E3 $ALPX,11,1.7E-5 /COM MAT,8 Center Stack Casing EX,8,200e9, $DENS,8,12.248E3 $ALPX,8,1.7E-5 !per Jan 17 email from A.Brooks NUXY,8,.3

  6. NSTX CSU Seismic Analysis Response Spectra Modal Analysis The last step is a macro created by the ANSYS script that combines the individual modal responses multiplied by their participation factor. /input,file,mcom. In the analysis performed for this calculation there is a difference between database created by reading the db file and the database from the results file. The file.mcom script should be run after the /post1 and set,1,1 commands to restore the proper database for the solution phase. file.mcom /COM,ANSYS RELEASE 13.0 UP20101012 12:49:19 01/23/2011 /COM, file.mcom LCOPER,ZERO LCDEFI,1, 1, 1 LCFACT,1, -0.217989 LCASE,1 LCOPER,SQUARE LCDEFI,1, 1, 2 LCFACT,1, -0.564958 LCOPER,ADD,1,MULT,1 LCDEFI,1, 1, 3 LCFACT,1, 0.405109 LCOPER,ADD,1,MULT,1 LCDEFI,1, 1, 4 LCFACT,1, 0.435993E-01 LCOPER,ADD,1,MULT,1 LCDEFI,1, 1, 5 LCFACT,1, -0.130370E-01 LCOPER,ADD,1,MULT,1 LCDEFI,1, 1, 6 LCFACT,1, -0.562580E-02 LCOPER,ADD,1,MULT,1 LCDEFI,1, 1, 7 LCFACT,1, -0.352451E-02 LCOPER,ADD,1,MULT,1 LCDEFI,1, 1, 8 LCFACT,1, 0.177986E-02 LCOPER,ADD,1,MULT,1 LCDEFI,1, 1, 11 LCFACT,1, 0.590136E-03 LCOPER,ADD,1,MULT,1 LCDEFI,1, 1, 13 LCFACT,1, 0.109637E-02 LCOPER,ADD,1,MULT,1 LCOPER,SQRT /solu antype,modal !modopt,subsp,8 ! this hung during solution modopt,lanb,24 Solve $save $fini /solu antype, spectrum $spopt,sprs,24,yes svtyp,2,2.0*9.8 $sed,1,0,0 FREQ,.55555556,.58823529,.625,.66666667,.71428571,.76923077,.83333333,.90909091,1 FREQ,1.1111111,1.25,1.4285714,1.6666667,2,2.5,3.3333333,4.1666667,5 FREQ,20,100 sv,0.0,.047,.05,.053,.057,.061,.065,.071,.077,.085 sv,0.0,.095,.106,.122,.142,.17,.213,.284,.36,.36 sv,0.0,.36,.144 sv,0.05,.031,.033,.035,.038,.041,.043,.047,.051,.057 sv,0.05,.063,.071,.081,.095,.113,.142,.189,.24,.24 sv,0.05,.24,.096 Solve $save $fini /solu antype,modal $mxpand,24,,,yes modopt,lanb,24 $solve $save $fini /solu antype,spectrum $srss,,disp $solve $save fini

  7. [14] SEISMIC ANALYSIS OF THE NATIONAL COMPACT STELLERATOR Experiment (NCSX) PSFC/JA-04-25Peter H. Titus May 17 2004 Stress – SRSS of All Loads Run #7 First Mode Mode 7 Run #4 Mode 8 Run #4

  8. .5g + deadweight Static Analysis Response Spectra Modal Analysis

  9. Seismic Stresses in Plate Elements

  10. Seismic Stresses in Plate Elements

  11. Bottom Bellows Static .5g Lateral Analysis Mode 4 Bottom Bellows Modal Analysis

  12. Influence Coefficient Input Without and With Plasma Input pfcu 33,10,1,1.1 1,0,5.88,-5.88,0,5.88,-5.88,0,5.88,-5.88,0 2,0,5.808,-5.808,0,5.808,-5.808,0,5.808,-5.808,0 3,0,5.76,-5.76,0,5.76,-5.76,0,5.76,-5.76,0 4,0,5.664,-5.664,0,5.664,-5.664,0,5.664,-5.664,0 5,.359832,.37722,.371112,.390576,.408816,-.354936,-.30714,-.258432,.476532,5.06088e-30 6,-.010924,.04144,-.10572,-.0533,-5.5200006e-4,.146874,.171922,.196724,-.112594,-7.3322e-31 7,.0236286,.0969048,-.064197,.007002,.0787428,.2412108,.2894778,.3373632,-.1209546,-5.64624e-31 8,.1054018,.1716624,.0594398,.1269534,.1944908,-.0277578,.0517062,.1312458,.076958,1.50325e-30 9,.1054018,.1716624,.0594398,.1269534,.1944908,-.0277578,.0517062,.1312458,.076958,1.50325e-30 10,-.061488,-.0466655,-.0786457,-.0633668,-.0486668,-.0775285,-.0637441,-.0499366,-.0427539,-2.85152e-31 11,-.070272,-.053332,-.0898808,-.0724192,-.0556192,-.088604,-.0728504,-.0570704,-.0488616,-3.25888e-31 12,-.061488,-.0466655,-.0786457,-.0633668,-.0486668,-.0775285,-.0637441,-.0499366,-.0427539,-2.85152e-31 13,-.070272,-.053332,-.0898808,-.0724192,-.0556192,-.088604,-.0728504,-.0570704,-.0488616,-3.25888e-31 14,-.0047808,-.0051176,-.0089808,-.0095296,-.010106,.0155472,.0155812,.015618,-.0567688,-5.69548e-31 15,-.0047808,-.0051176,-.0089808,-.0095296,-.010106,.0155472,.0155812,.015618,-.0567688,-5.69548e-31 16,-.0107568,-.0115146,-.0202068,-.0214416,-.0227385,.0349812,.0350577,.0351405,-.1277298,-1.281483e-30 17,-.0047808,-.0051176,-.0089808,-.0095296,-.010106,.0155472,.0155812,.015618,-.0567688,-5.69548e-31 18,-.005976,-.006397,-.011226,-.011912,-.0126325,.019434,.0194765,.0195225,-.070961,-7.11935e-31 19,-.0095616,-.0102352,-.0179616,-.0190592,-.020212,.0310944,.0311624,.031236,-.1135376,-1.139096e-30 20,-.2654436,-.2539032,-.268596,-.2571468,-.2447724,-.3083028,-.297246,-.2862444,-.214518,-2.028324e-30 21,-.2654436,-.2539032,-.268596,-.2571468,-.2447724,-.3083028,-.297246,-.2862444,-.214518,-2.028324e-30 22,-.2654436,-.2539032,-.268596,-.2571468,-.2447724,-.3083028,-.297246,-.2862444,-.214518,-2.028324e-30 23,-.2654436,-.2539032,-.268596,-.2571468,-.2447724,-.3083028,-.297246,-.2862444,-.214518,-2.028324e-30 24,-.070272,-.053332,-.0898808,-.0724192,-.0556192,-.088604,-.0728504,-.0570704,-.0488616,-3.25888e-31 25,-.061488,-.0466655,-.0786457,-.0633668,-.0486668,-.0775285,-.0637441,-.0499366,-.0427539,-2.85152e-31 26,-.061488,-.0466655,-.0786457,-.0633668,-.0486668,-.0775285,-.0637441,-.0499366,-.0427539,-2.85152e-31 27,-.070272,-.053332,-.0898808,-.0724192,-.0556192,-.088604,-.0728504,-.0570704,-.0488616,-3.25888e-31 28,.1054018,.1716624,.0594398,.1269534,.1944908,-.0277578,.0517062,.1312472,.076958,1.50325e-30 29,.1054018,.1716624,.0594398,.1269534,.1944908,-.0277578,.0517062,.1312472,.076958,1.50325e-30 30,.0236286,.0969048,-.064197,.007002,.0787428,.2412108,.2894778,.3373632,-.1209546,-5.64624e-31 31,-.010924,.04144,-.10572,-.0533,-5.5200006e-4,.146874,.171922,.196724,-.112594,-7.3322e-31 32,1.7502667e-2,7.1781333e-2,-4.7553333e-2,5.1866666e-3,.058328,.17867467,.214428,.24989867,-.089596,-4.1824e-31 33,0,0,0,0,0,0,0,0,0,0 Data Set 11 pfcu 33,16,11,1.0 1 , 245 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 2 , 242 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 3 , 240 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 4 , 236 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 5 , 0 , 120 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 6 , 0 , 0 , 108 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 7 , 0 , 0 , 0 , 162 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 8 , 0 , 0 , 0 , 0 , 14 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 9 , 0 , 0 , 0 , 0 , 14 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 10 , 0 , 0 , 0 , 0 , 0 , 7 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 11 , 0 , 0 , 0 , 0 , 0 , 8 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 12 , 0 , 0 , 0 , 0 , 0 , 7 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 13 , 0 , 0 , 0 , 0 , 0 , 8 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 14 , 0 , 0 , 0 , 0 , 0 , 0 , 4 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 15 , 0 , 0 , 0 , 0 , 0 , 0 , 4 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 16 , 0 , 0 , 0 , 0 , 0 , 0 , 9 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 17 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 4 , 0 ,0 18 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 5 , 0 ,0 19 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 8 , 0 ,0 20 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 12 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 21 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 12 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,0 22 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 12 ,0 23 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 12 ,0 24 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 8 , 0 , 0, 0 25 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 7 , 0 , 0 ,0 26 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 7 , 0 , 0 ,0 27 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 8 , 0 , 0 ,0 28 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 14 , 0 , 0 , 0 ,0 29 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 14 , 0 , 0 , 0 ,0 30 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 162 , 0 , 0 , 0 , 0 ,0 31 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 180 , 0 , 0 , 0 , 0 , 0 ,0 32 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 120 , 0 , 0 , 0 , 0 ,0 33 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ,1000 No Plasma 28,.1054018,.1716624,.0594398,.1269534,.1944908,-.0277578,.0517062,.1312472,.076958,1.50325e-30 29,.1054018,.1716624,.0594398,.1269534,.1944908,-.0277578,.0517062,.1312472,.076958,1.50325e-30 30,.0236286,.0969048,-.064197,.007002,.0787428,.2412108,.2894778,.3373632,-.1209546,-5.64624e-31 31,-.010924,.04144,-.10572,-.0533,-5.5200006e-4,.146874,.171922,.196724,-.112594,-7.3322e-31 32,1.7502667e-2,7.1781333e-2,-4.7553333e-2,5.1866666e-3,.058328,.17867467,.214428,.24989867,-.089596,-4.1824e-31 33 , 2 , 2 , 2 , 2 , 2 , 2, 2 , 2 , 2 , 2 2 MA Plasma

  13. PF5u Influence Coefficient load file Minus the TFON load file

  14. Upper Corner TF Shear Coefficients Full Global Model Influence Coefficients For PF Coefficients per kA and IP Coefficient per MA – Divide values by 1000 TF Upper-Inner Corner Torsional Shear, June 3 2010 Scenario OH +13/-24 kA

  15. Upper Corner TF Shear Coefficients Full Global Model Influence Coefficients Fixed at Umbrella Structure Single TF Model Influence Coefficients Fixity at Umbrella Structure Suppresses the Contributions of Outboard Coils For PF Coefficients per kA and IP Coefficient per MA – Divide values by 1000

  16. Plasma4 Quench Analysis of the Vessel PP and Full Vessel Have not Been Integrated

  17. Static Dynamic P4 Quench Stresses are not Significant on the Vessel (Content will be added to NSTXU-CALC-12-01-00

  18. seal 0 squa 1 grprel 1,1 r 1,1,.000767 plto Conversion of plate elements to Solids

  19. The Global Model Currently Assumes Flat Spoke Assemblies Top and Bottom ~.003 in Lower Bent Spoke Assembly ~.008 in

  20. Suggested Added Ring Section

  21. .0045 in

  22. No plasma No plasma title Run#%runn%,nstxU,Therm+TFON,%tffield%T /input,tfon,mod solve Save *do,ls,1,9 /title Run#%runn%,nstxU,Therm+TFON,data set #990%ls%,%tffield%T /input,990%ls%,mod solve save *enddo *do,ls,1,9 /title Run#%runn%,nstxU,Therm+TFON,data set #990%ls%,%tffield%T With Plasma /input,ip0%ls%,mod solve save *enddo *do,ls,10,20 /title Run#%runn%,nstxU,Therm+TFON,data set #99%ls%,%tffield%T /input,99%ls%,mod solve save *enddo *do,ls,10,20 /title Run#%runn%,nstxU,Therm+TFON,data set #99%ls%,%tffield%T With Plasma /input,ip%ls%,mod solve save *enddo *do,ls,21,30 /title Run#%runn%,nstxU,Therm+TFON,data set #99%ls%,%tffield%T /input,99%ls%,mod solve save *enddo W/plasma W/plasma Vessel Bending Stresses at the PF5 Supports at the Chosen Point are Lower With Plasma No plasma W/plasma No plasma W/plasma PF5 Bending Stresses are Higher With Plasma

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