*-------------------------------------------------------------------- * TEST CASE TCDR16 * DB-VHTR Fuel Block Lattice calculation * Fresh fuel TRU loading * Author : V. Descotes * Core corner block(6,1), no BP, no CR. *-------------------------------------------------------------------- * *-------------------------------------------------------------------- * Define STRUCTURES and MODULES used *-------------------------------------------------------------------- LINKED_LIST LIBRARY LIBRARY2 GEOM TRACK SYS FLUX ; SEQ_BINARY TRACK_FIL ; MODULE GEO: LIB: ASM: FLU: USS: EXCELT: MCCGT: END: ; PROCEDURE assertS ; *-------------------------------------------------------- * GEOMETRY *-------------------------------------------------------- * ---- * F = Fuel cell * C = coolant hole cell (large) * K = coolant hole cell (small) * G = Full density graphite cell * J = Reduced density graphite cell * ---- GEOM := GEO: :: HEX 1 EDIT 1 HBC COMPLETE REFL CELL F0 ::: F0 := GEO: HEXCEL 2 SIDE 1.08542 RADIUS 0.0 0.6225 0.6350 SECT -1 MIX 9 9 9 9 9 9 7 7 7 7 7 7 8 8 8 8 8 8 ; * *--------------------------------------------------------- * SPHERICAL MICRO-STRUCTURES * * NMISTR = NUMBER OF MICRO STRUCTURE TYPES IN REGION * NMILG = NUMBER OF MICRO STRUCTURE REGIONS * NS = ARRAY OF SUB REGIONS IN THE MICRO STRUCTURES; LEN=NMILG * RS = RADIUS OF MICROS STRUCTURES; LEN=NS(I); I=1,NMISTR * milie = COMPOSITION OF EACH shell OF MICRO STRUCTURE; LEN=NMISTR; * !!!!!!!! milie #'s ARE > THAN MIX #'S !!!!!!!! * mixdil = BASE COMPOSITION OF EACH REGION; LEN=NMILG * fract = MICROSTRUCTURE TYPE VOLUME FRACTION IN REGION LEN=NMILG * mixgr = LIBRARY MIXTURES FOR EACH MICROSTRUCTURE SHELL; LEN=NS(I) * NMISTR, NMILG BIHET SPHE 1 1 (* NS *) 5 (* RS *) 0.0 0.0100 0.0220 0.0260 0.0295 0.0335 (* milie *) 9 (* mixdil *) 1 (* loop over NMISTR *) (* fract *) 0.175016 (* mixgr *) 2 3 4 5 6 ; *-------------------------------------------------------------------- * Use EXCELT-MCCGT, USS, ASM and FLU for flux solution *-------------------------------------------------------------------- *** * Tracking EXCELT-MCCGT *** TRACK TRACK_FIL := EXCELT: GEOM :: EDIT 1 MAXR 50000 ANIS 1 ALLG QUAB 5 HEBE PISO TRAK TISO 4 10.0 ; TRACK := MCCGT: TRACK TRACK_FIL GEOM :: EDIT 0 LCMD 3 EPSI 5E-5 MAXI 100 KRYL 10 SCR 1 AAC 1 TMT ; *-------------------------------------------------------------------- * CREATION OF THE LIBRARY *-------------------------------------------------------------------- LIBRARY := LIB: :: EDIT 0 NMIX 8 CTRA APOL ANIS 2 SUBG MIXS LIB: DRAGON FIL: DLIB_J2 *---- * Mixtures for fuel cell F0 *---- * Graphite matrix MIX 1 293.6 GRAB = 'C0_GR' 8.524E-02 * Fuel Kernel MIX 2 293.6 O16 = 'O16' 4.436E-02 NP27 = 'Np237' 1.522E-03 1 PU38 = 'Pu238' 6.464E-04 1 PU39 = 'Pu239' 1.099E-02 1 PU40 = 'Pu240' 5.084E-03 1 PU41 = 'Pu241' 1.937E-03 1 PU42 = 'Pu242' 1.074E-03 1 AM41 = 'Am241' 6.163E-04 1 AM42 = 'Am242m' 4.385E-06 1 AM43 = 'Am243' 3.057E-04 1 * Porous C buffer MIX 3 293.6 GRAB = 'C0_GR' 5.265E-02 * IPyC MIX 4 293.6 GRAB = 'C0_GR' 9.526E-02 * SiC coating layer MIX 5 293.6 SI0 = 'Si0' 4.402E-02 C12 = 'C0' 4.772E-02 * OPyC MIX 6 293.6 GRAB = 'C0_GR' 9.526E-02 * Helium Coolant surrounding fuel MIX 7 293.6 HE4 = 'He4' 7.0000E-04 * Block Graphite (full density surrounding fuel) MIX 8 293.6 GRAB = 'C0_GR' 8.774E-02 ; *--- * Self Shielding calculation *--- LIBRARY2 := USS: LIBRARY TRACK TRACK_FIL :: EDIT 0 PASS 2 ARM ; *--- * Multigroup Flux Calculation *--- SYS := ASM: LIBRARY2 TRACK TRACK_FIL :: EDIT 0 ARM PNOR HELI ; FLUX := FLU: SYS LIBRARY2 TRACK TRACK_FIL :: EDIT 1 TYPE K P1 EXTE 300 1E-5 THER 10 1E-5 ; assertS FLUX :: 'K-EFFECTIVE' 1 1.144789 ; ECHO "test TCDR16 completed" ; END: ; QUIT "LIST" .