14., 1.0, -1.0 *DEPVAR 29 ** *USER SUBROUTINE, INPUT=/wms12/weiqi/umats/poly/d-chaboche.f ** ** first loading, cycle 1 ** *STEP, INC=100000000, NLGEOM ***STATIC *VISCO, CETOL=1.0E-10 .01, 100., , 0.1 ** ** *BOUNDARY,OP=NEW 12, 1, 3, .00000E+00 45, 1, 3, .00000E+00 46, 1, 3, .00000E+00 15, 1, 3, .00000E+00 fuss, 1, 3, .00000E+00 ** ** rotations ** -48-
*AMPLITUDE, NAME=CYCLEONE, DEFINITION=TABULAR, TIME=STEP TIME 0., 0., 10., .05415, 100., 1., 900000000., 1. ** *DLOAD, OP=NEW, AMPLITUDE=CYCLEONE blade, CENTRIF, 444000., 35., 0., 0., 0., 0., 1. **entspricht Drehzahl von 40000/min oder 666/sec ** *RESTART, WRITE, FREQUENCY=10000000 ** *NODE FILE, FREQ=0 *EL FILE, POS=INTEG, FREQ=0 S, E, SDV *EL PRINT,POS=INTEG, FREQ=0 *NODE PRINT, FREQ=0 *PRINT, FREQ=0 *END STEP *** *** *** *STEP, INC=100000000 ***STATIC *VISCO, CETOL=1.0E-10 0.1, 3600., , 10. ** *EL FILE, POS=INTEG, FREQ=0 *NODE FILE, FREQ=0 *PRINT, FREQ=0 *END STEP *** *** *** *STEP, INC=100000000 *VISCO, CETOL=1.0E-10 50., 720000., , 50. *RESTART, WRITE, FREQUENCY=1440 ** *EL FILE, POS=INTEG, FREQ=0 *NODE FILE, FREQ=0 *PRINT, FREQ=0 *END STEP *** *** ** *STEP, INC=100000000 *VISCO, CETOL=1.0E-10 200., 720000., , 200. ** *RESTART, WRITE, FREQUENCY=360 ** *EL FILE, POS=INTEG, FREQ=0 *NODE FILE, FREQ=0 *PRINT, FREQ=0 *END STEP *** ** *STEP, INC=100000000 *VISCO, CETOL=1.0E-10 400., 72000000., , 400. ** *RESTART, WRITE, FREQUENCY=180 ** *EL FILE, POS=INTEG, FREQ=0 *NODE FILE, FREQ=0 -49-
- Page 1 and 2: Technical Note GKSS/WMS/01/5 intern
- Page 4 and 5: 0. Nomenclature 3 1. Introduction 7
- Page 6 and 7: R ∞ Wi Z I , Z D Zij 6 saturated
- Page 8 and 9: W internal variable, eq. (20b) four
- Page 10 and 11: where S is the CAUCHY stress tensor
- Page 12 and 13: 12 0 for x ≤ xm 1 h(x) = 2 1− c
- Page 14 and 15: flow rule: E Ý i = p Ý ˜ S ′
- Page 16 and 17: 16 −1 −1 D1 = 0 , L1 = 0, Z i1
- Page 18 and 19: parameters of Tables 2 and 3, and t
- Page 20 and 21: 20 Fig. 1. Experiments and model pr
- Page 22 and 23: 22 Fig. 3. Contour plots of the max
- Page 24 and 25: 24 Fig. 5. Contour plots of directi
- Page 26 and 27: 26 Fig. 6. FE-mesh and loading cond
- Page 28 and 29: 28 Fig. 13. FE-mesh and loading con
- Page 30 and 31: proove that the model performs well
- Page 33 and 34: 6. References AI, S.H.; LUPINC, V.
- Page 35 and 36: 7. Appendices: ABAQUS-Inputfiles 7.
- Page 37 and 38: ** auflagerung ** *BOUNDARY, OP=NEW
- Page 39 and 40: ** E, nu, Do, n, K1, K2, K3, m1 149
- Page 41 and 42: ** ====== 2. load ein ** *STEP, INC
- Page 43 and 44: 7.3 Appendix 3: Single crystal plat
- Page 45 and 46: *NODE FILE, FREQUENCY=0 *EL FILE, F
- Page 47: 7.4 Appendix 4: TiAl turbine blade
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