' CONSTANTS NAMES FOR FORCE REDUCTION PROGRAM ' ======================================================================================== ' ' ' Constants Array Indexes Description ' ---------------------------------------------------- ' ' CORRECTION SWITCHES BCMETHOD = 1 ' Blockage method: 0 = no blockage corr, 1 = solid only, 2 = classic (old UWAL), 3 = Shindo WCMETHOD = 2 ' Wall correction method: 0 = no wall corr, 1 = approximate, 2 = classic (old UWAL) WTMETHOD = 3 ' Weight tare type: 0 = do not apply, 1 = full, 2 = 3-pt tares USEWOZ = 4 ' True (-1) = subtract WOZ values for force data, False = don't subtract WOZ values. ALPHAREF = 5 ' Which alpha to use for DR: 0 = encoder, 1 = accelerometer PITCHYAW = 6 ' Run type switch, 1 = pitch, 2 = yaw ' MISCELLANEOUS MODEL INFORMATION CA = 7 ' Actual cross-sectional area of the test section, sq ft. = CA_ref - fillet area C_REF = 8 ' Reference cross-sectional area of the test section, sq. ft. (rectangular) TAILON = 9 ' Tail switch, 0 = off, 1 = on. GPHEIGHT = 10 ' Height of the ground plane, if installed INVERTED = 11 ' Inverted switch, 0 = upright, 1 = inverted DATAAVG = 12 ' Data averaging switch, 0 = no averaging, 1 = avg scan pos, 2 = avg tps ' WALL CORRECTIONS LIFT_RUN = 13 ' Run that has lift values for use in sizing wall corrections DELW = 14 ' Wall correction constant for the wing ' TARES WTARERUN = 15 ' Run number of weight tare NONAERO = 16 ' Is this model a non-aero test? 1 = yes, 0 = no (aero test = airplane-like objects) BLANK = 17 BLANK = 18 ' GEOMETRY CONSTANTS ACWX = 19 ' Horizontal distance of wing AC to trunnion, in (added 2/10/99 for better delas, delw calc) ACWZ = 20 ' Vertical distance from wing AC to trunnion, in (added 2/10/99 for better delas, delw calc) CROOT = 21 ' Root chord in (added 2/10/99 for better delas, delw calc) CTIP = 22 ' Tip chord in (added 2/10/99 for better delas, delw calc) SW = 23 ' Surface area of the wing ft^2 MAC = 24 ' Mean Aerodynamic Chord in B_REF = 25 ' Wing span, reference in B_ACT = 26 ' Wing span, actual in AR_ACT = 27 ' Actual aspect ratio = b_act * b_act / Sw AR = 28 ' Aspect ratio = b_ref * b_ref / Sw CONSTRUN = 29 ' Current run number for rebuilding the binary data (if necessary) LTO = 30 ' Horizontal distance from wing a.c. to horizontal tail a.c. (in) TTO = 31 ' Vertical distance from wing a.c. to horizontal tail a.c. (in) XDIST = 32 ' Horizontal distance from trunnion to balance moment center (in) ZDIST = 33 ' Vertical distance from trunnion to balance moment center (in) ' MOMENT TRANSFERS MOMENTS = 34 ' Number of moment transfers MMC1 = 35 ' Model Moment Center (%MAC), #1 MMC2 = 36 ' Model Moment Center (%MAC), #2 MMC3 = 37 ' Model Moment Center (%MAC), #3 MMC4 = 38 ' Model Moment Center (%MAC), #4 MMC5 = 39 ' Model Moment Center (%MAC), #5 GAMMA1 = 40 ' Angle of rotation from tunnel centerline to MMC1 GAMMA2 = 41 ' Angle of rotation from tunnel centerline to MMC2 GAMMA3 = 42 ' Angle of rotation from tunnel centerline to MMC3 GAMMA4 = 43 ' Angle of rotation from tunnel centerline to MMC4 GAMMA5 = 44 ' Angle of rotation from tunnel centerline to MMC5 A1 = 45 ' Distance from the trunnion to MMC1, inches A2 = 46 ' Distance from the trunnion to MMC2, inches A3 = 47 ' Distance from the trunnion to MMC3, inches A4 = 48 ' Distance from the trunnion to MMC4, inches A5 = 49 ' Distance from the trunnion to MMC5, inches LH1 = 50 ' Horizontal distance from MMC1 to the horizontal tail a.c. LH2 = 51 ' Horizontal distance from MMC2 to the horizontal tail a.c. LH3 = 52 ' Horizontal distance from MMC3 to the horizontal tail a.c. LH4 = 53 ' Horizontal distance from MMC4 to the horizontal tail a.c. LH5 = 54 ' Horizontal distance from MMC5 to the horizontal tail a.c. ' BLOCKAGE CORRECTIONS BC_KA = 55 ' Shape factor for airfoil sections on the model BC_KB = 56 ' Shape factor for bodies of revolution on the model BC_KW = 57 ' Wing separation factor BC_VA = 58 ' Volume of airfoils on the model (ft^3) BC_VB = 59 ' Volume of bodies of revolution on the model (ft^3) BC_A1 = 60 ' Factor based on aspect ratio BC_A2 = 61 ' Factor based on flaps ' AUXILIARY TEST CONSTANTS ' Elements 62 to 100 are for test specific constants) BLANK = 62 BLANK = 63 BLANK = 64 BLANK = 65 BLANK = 66 BLANK = 67 BLANK = 68 BLANK = 69 BLANK = 70 BLANK = 71 BLANK = 72 BLANK = 73 BLANK = 74 BLANK = 75 BLANK = 76 BLANK = 77 BLANK = 78 BLANK = 79 BLANK = 80 BLANK = 81 BLANK = 82 BLANK = 83 BLANK = 84 BLANK = 85 BLANK = 86 BLANK = 87 BLANK = 88 BLANK = 89 BLANK = 90 BLANK = 91 BLANK = 92 BLANK = 93 BLANK = 94 BLANK = 95 BLANK = 96 BLANK = 97 BLANK = 98 BLANK = 99 BLANK = 100