#WARNING: DO NOT DELETE ANY LINE STARTING WITH # sign.
#THIS IS AN EXAMPLE FILE THAT SHOULD BE USED WITH MIXED-ELEMENT USM3D
#USE THIS FILE TO SPECIFY INPUT FOR BC10102, BC10101, BC10111,
# BC11002, AND BC11003
#BC 10101 IS SIMILAR TO ENGINE INTAKE BC (101, 201, 301...)
#BC 10102 IS SIMILAR TO ENGINE EXHAUST BC (102, 202, 302...)
#BC 10111 IS SIMILAR TO SINK BC (111, 211, 311...)
#BC 11002 IS SIMILAR TO OUTFLOW BC 1002 WITH SPECIFIED PRESSURE
#BC 11003 IS AN OUTFLOW BC WITH SPECIFIED MACH NUMBER
########WARNING:##### BC 10501 AND BC10502 ARE NOT AVAILABLE AT THIS TIME
#BC 10501 IS SIMILAR TO ROTOR BC (501, 601, 701...), NO INPUT REQUIRED.
#BC 10502 IS MOSTLY SIMILAR TO ROTOR BC (502, 602, 702...)
#FIRST TWO COLUMNS FOR EACH ROW WILL BE SAME
#FIRST COLUMN TO SPECIFY PATCH NUMBER
#SECOND COLUMN TO SPECIFY BOUNDARY CONDITION (BC) NUMBER
#VALUES IN SUBSEQUENT COLUMN WILL VARY DEPENDING ON BC NUMBER
#THIRD COLUMN SPECIFIES NUMBER OF INPUT VALUES FOR THE SPECIFIC PATCH
#FOURTH COLUMN ONWARD EACH OF THE NUMBER OF INPUT VALUES ARE SPECIFIED
#EXAMPLES OF NEWLY ADDED BCS ARE GIVEN BELOW.
#PATCH 7 AND 9 BELOW ARE SET TO BC 10102. THIS BC NEEDS SPECIFICATION
#OF NINE VALUES, NAMELY, FUEL_FRACTION, GAMMAJ, PJET, P0JET, RRATIO,
#T0JET, VEC(1), VEC(2), VEC(3)
#7 10102 9 0.02 1.3 0.71430 1.42857 0.77400 3.17390 1.0 0.0 0.0
#9 10102 9 0.00 1.4 0.71430 1.00000 1.00000 1.02000 1.0 0.0 0.0
#PATCH 14 BELOW IS SET TO BC10101. THIS BC NEEDS IDs OF THE EXHAUST BC
#PATCHES TO WHICH THIS PATCH IS COUPLED. PATCH 14 IS CONNECTED TO
#TWO EXHAUST BC PATCHES, NAMELY, PATCH 7 AND PATCH 9.
#14 10101 2 7 9
#PATCH 17 BELOW IS SET TO BC10111. ONLY MASS FLOW VALUE (NON_DIMESIONALIZED
#BY RHO_INF*CSOUND_INF) NEEDS TO BE SPECIFIED FOR THIS BC
#17 10111 1 5.7
#PATCH 22 AND 32 BELOW ARE SET TO BC10502. THIS BC NEEDS SPECIFICATION
#OF AT LEAST NINE VALUES FOR BOTH UNIFORM AND RADIALLY-VARYING JUMP
#CONDITIONS. FOR RADIALLY-VARYING JUMP CONDITIONS, MORE DATA ARE NEEDED
#AS SHOWN BELOW FOR PATCH 32. THE NINE VALUES ARE ROTOR_OUTER_RADIUS,
#X-COORDINATE_OF_ROTOR_CENTER, Y-COORDINATE_OF_ROTOR_CENTER,
#Z-COORDINATE_OF_ROTOR_CENTER, ADVANCE_RATIO, THRUST_COEFFICIENT,
#TORQUE_COEFFICIENT, ROTATIONAL_DIRECTION, TYPE_OF_ROTOR_JUMP_CONDITION.
#FOR THE PATCH THAT HAS RADIALLY-VARYING JUMP CONDITIONS, THE NEEDED
#INPUT VALUES ARE: NUMBER_OF_DATA_POINTS_FOR_RADIAL_VARIATION_OF_THRUST,
#ARRAY_OF_RADIAL_LOCATIONS_FOR_THRUST, ARRAY_OF_DCTDR,
#NUMBER_OF_DATA_POINTS_FOR_RADIAL_VARIATION_OF_TORQUE,
#ARRAY_OF_RADIAL_LOCATIONS_FOR_TORQUE, ARRAY_OF_DCQDR
#22 10502 9 24.0 0.0 0.0 0.0 0.2 0.00861 0.002 1 0
#32 10502 9 12.0 0.0 100.0 20.0 0.15 0.0043 0.001 0 1
#10
#0.168,0.350,0.500,0.600,0.700,0.800,0.900,0.950,0.975,1.000
#-0.0070,0.0379,0.1155,0.1958,0.2450,0.2563,0.1948,0.1195,0.0660,0.0
#10
#0.168,0.350,0.500,0.600,0.700,0.800,0.900,0.950,0.975,1.000
#0.0009,0.0131,0.0345,0.0575,0.0717,0.0746,0.0571,0.0363,0.0218,0.0
#PATCH 36, 39 BELOW ARE SET TO BC11002. ONLY BACK PRESSURE
#NEEDS TO BE SPECIFIED FOR THIS BC. THEREFORE, THIRD COLUMN WILL
#HAVE VALUE 1 AND FOURTH COLUMN WILL HAVE VALUE OF BACK PRESSURE.
#36 11002 1 0.74
#39 11002 1 0.65
#PATCH 47 BELOW IS SET TO BC11003. ONLY MACH NUMBER VALUE
#NEEDS TO BE SPECIFIED FOR THIS BC.
#47 11003 1 0.4
#WARNING: DO NOT DELETE ANY LINE STARTING WITH # sign.
3 11002 1 0.7
4 10102 9 0.0 1.4 1.40 1.42857 1.0 3.17390 0.0 0.0 0.0
