\begintext HUYGENS AERODYNAMIC DATABASE REFERENCE: HUYGENS PROBE Probe data synthesis for Instruments Technical Note and Excel Spread Sheets from January 2005 ======================================================================= FREE MOLECULAR FLOW (FMF) REGIME ======================================================================= KN > 10 (KN=1.25*GAMMA*Ma/Re) \begindata HUY_AOA_FMF=(0.0,5.0,10.0,20.0,30.0) \begintext FMF AXIAL FORCE COEFFICIENT \begindata HUY_FMF_CA=(2.09,2.075,2.033,1.864,1.599) \begintext FMF NORMAL FORCE COEFFICIENT \begindata HUY_FMF_CN=(0.000,0.138,0.272,0.514,0.697) \begintext FMF Database Dimension \begindata HUY_FMF_Nr=(5) \begintext ======================================================================= TRANSITIONAL FLOW REGIME ======================================================================= AOA array in [deg] Knudsen Number Array in 10LOG \begindata HUY_AOA_TRANS=(0.0,5.0,10.0,20.0,30.0) HUY_KNUD_TRANS=(-3.0000,-2.6990,-2.5229,-2.3010,-2.1549,-2.0000,-1.8239,-1.6990, -1.6021,-1.3979,-1.3010,-1.2218,-1.0969,-1.0000,-0.6990,-0.5229,-0.3010,-0.1549, -0.0458,0.0899,0.3010,0.4771,0.6990,0.8451,0.9542,1.0000) \begintext Axial Force Coefficient for Transitional Flow Regime \begindata HUY_TRANS_CA=( 1.4780,1.4865,1.4992,1.5230,1.5430,1.5676,1.5995,1.6243,1.6446,1.6899, 1.7123,1.7310,1.7607,1.7840,1.8557,1.8960,1.9437,1.9725,1.9925,2.0151, 2.0450,2.0646,2.0815,2.0877,2.0898,2.0900, 1.4565,1.4651,1.4780,1.5019,1.5222,1.5471,1.5793,1.6044,1.6249,1.6707, 1.6933,1.7121,1.7422,1.7658,1.8382,1.8789,1.9271,1.9563,1.9764,1.9993, 2.0296,2.0493,2.0664,2.0727,2.0748,2.0750, 1.4172,1.4258,1.4386,1.4624,1.4826,1.5074,1.5395,1.5644,1.5849,1.6304, 1.6530,1.6717,1.7017,1.7251,1.7972,1.8378,1.8858,1.9148,1.9349,1.9576, 1.9878,2.0074,2.0244,2.0307,2.0328,2.0330, 1.2481,1.2567,1.2695,1.2933,1.3135,1.3383,1.3704,1.3954,1.4158,1.4614, 1.4839,1.5027,1.5326,1.5561,1.6282,1.6688,1.7167,1.7458,1.7658,1.7886, 1.8188,1.8384,1.8554,1.8617,1.8638,1.8640, 1.0663,1.0737,1.0848,1.1054,1.1228,1.1443,1.1721,1.1937,1.2113,1.2508, 1.2703,1.2865,1.3124,1.3327,1.3950,1.4301,1.4716,1.4967,1.5141,1.5338, 1.5599,1.5769,1.5916,1.5970,1.5988,1.5990 ) \begintext Normal Force Coefficient for Transitional Flow Regime \begindata HUY_TRANS_CN=( 0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000, 0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000, 0.0000,0.0000,0.0000,0.0000,0.0000,0.0000, 0.0240,0.0256,0.0280,0.0324,0.0361,0.0407,0.0466,0.0513,0.0550,0.0635, 0.0676,0.0711,0.0767,0.0810,0.0944,0.1019,0.1107,0.1161,0.1198,0.1240, 0.1296,0.1333,0.1364,0.1376,0.1380,0.1380, 0.0565,0.0595,0.0640,0.0723,0.0794,0.0881,0.0993,0.1080,0.1152,0.1311, 0.1390,0.1456,0.1561,0.1643,0.1895,0.2037,0.2205,0.2306,0.2377,0.2456, 0.2562,0.2630,0.2690,0.2712,0.2719,0.2720, 0.1236,0.1290,0.1371,0.1523,0.1650,0.1808,0.2011,0.2169,0.2299,0.2588, 0.2731,0.2850,0.3040,0.3188,0.3645,0.3902,0.4207,0.4391,0.4518,0.4662, 0.4853,0.4978,0.5086,0.5126,0.5139,0.5140, 0.1749,0.1822,0.1930,0.2133,0.2303,0.2514,0.2786,0.2997,0.3171,0.3557, 0.3748,0.3907,0.4161,0.4360,0.4971,0.5315,0.5722,0.5968,0.6138,0.6331, 0.6586,0.6753,0.6897,0.6951,0.6968,0.6970 ) \begintext Transitional Regime Database Dimension \begindata HUY_TRANS_AOA_Nr=(5) HUY_TRANS_Reg_Nr=(26) \begintext ======================================================================= CONTINUUM FLOW REGIME (HYPERSONIC AND SUPERSONIC) ======================================================================= APPLICABLE CONDITIONS: 21.8 > Ma > 1.5 3.4*104 > Re > 1.8*105 Angle of Attack in [DEG] \begindata HUY_AOA=(0.0,1.0,2.0,3.0,4.0,5.0,6.0,7.0,8.0,9.0,10.0, 11.0,12.0,13.0,14.0,15.0,16.0,17.0,18.0,19.0,20.0, 21.0,22.0,23.0,24.0,25.0,26.0,27.0,28.0,30.0,40.0, 50.0,60.0) \begintext Mach Number \begindata HUY_MA=(0.0,0.5,0.8,1.0,1.19,1.42,1.71,2.03,4.0,7.15,10.0,30.0,99.0) \begintext Axial force coefficients as function of the angle-of-attack and flow regime (i.e., Mach Number) \begindata HUY_CA=( 0.9349,0.9349,1.0322,1.1338,1.1827,1.3941,1.4646,1.4890,1.4834,1.4780,1.4780,1.4780,1.4780, 0.9385,0.9385,1.0305,1.134, 1.1844,1.3972,1.4673,1.4906,1.4809,1.4751,1.4751,1.4751,1.4751, 0.9398,0.9398,1.0286,1.1355,1.1874,1.4034,1.4699,1.4918,1.4775,1.4715,1.4715,1.4715,1.4715, 0.9393,0.9393,1.0266,1.1378,1.1908,1.4082,1.4714,1.4923,1.4739,1.4672,1.4672,1.4672,1.4672, 0.9346,0.9346,1.0259,1.1404,1.1936,1.4082,1.4722,1.4924,1.4701,1.4622,1.4622,1.4622,1.4622, 0.9269,0.9269,1.0262,1.1433,1.1947,1.4061,1.4734,1.4925,1.4654,1.4565,1.4565,1.4565,1.4565, 0.9213,0.9213,1.0258,1.1444,1.1942,1.4063,1.4748,1.4926,1.4597,1.4500,1.4500,1.4500,1.4500, 0.9182,0.9182,1.0249,1.1432,1.1940,1.4095,1.4751,1.4919,1.4525,1.4429,1.4429,1.4429,1.4429, 0.9157,0.9157,1.0243,1.1432,1.1951,1.4137,1.4747,1.4906,1.4444,1.4350,1.4350,1.4350,1.4350, 0.9139,0.9139,1.0241,1.1453,1.1971,1.4172,1.4744,1.4888,1.4355,1.4264,1.4264,1.4264,1.4264, 0.9119,0.9119,1.0237,1.1461,1.1990,1.4202,1.4740,1.4868,1.4251,1.4172,1.4172,1.4172,1.4172, 0.9098,0.9098,1.0191,1.1484,1.2019,1.4232,1.4732,1.4843,1.4131,1.4032,1.4032,1.4032,1.4032, 0.9079,0.9079,1.0125,1.1539,1.2060,1.4259,1.4719,1.4816,1.3997,1.3885,1.3885,1.3885,1.3885, 0.9054,0.9054,1.0094,1.1580,1.2083,1.4277,1.4696,1.4781,1.3851,1.3731,1.3731,1.3731,1.3731, 0.9027,0.9027,1.0083,1.1593,1.2083,1.4285,1.4659,1.4733,1.3697,1.3571,1.3571,1.3571,1.3571, 0.8994,0.8994,1.0059,1.1620,1.2091,1.4283,1.4615,1.4674,1.3541,1.3405,1.3405,1.3405,1.3405, 0.8951,0.8951,1.0032,1.1679,1.2119,1.4274,1.4563,1.4607,1.3378,1.3232,1.3232,1.3232,1.3232, 0.8901,0.8901,1.0009,1.1713,1.2131,1.4256,1.4505,1.4530,1.3207,1.3053,1.3053,1.3053,1.3053, 0.8845,0.8845,0.9973,1.1732,1.2103,1.4227,1.4448,1.4443,1.3029,1.2868,1.2868,1.2868,1.2868, 0.8788,0.8788,0.9948,1.1795,1.2064,1.4190,1.4387,1.4345,1.2844,1.2677,1.2677,1.2677,1.2677, 0.8729,0.8729,0.9908,1.1872,1.2024,1.4148,1.4316,1.4237,1.2664,1.2481,1.2481,1.2481,1.2481, 0.8667,0.8667,0.9825,1.1914,1.1968,1.4098,1.4243,1.4118,1.2487,1.2321,1.2321,1.2321,1.2321, 0.8590,0.8590,0.9737,1.1912,1.1905,1.4039,1.4172,1.3988,1.2303,1.2156,1.2156,1.2156,1.2156, 0.8507,0.8507,0.9647,1.1885,1.1852,1.3975,1.4092,1.3850,1.2117,1.1986,1.1986,1.1986,1.1986, 0.8424,0.8424,0.9541,1.1869,1.1801,1.3905,1.3993,1.3701,1.1937,1.1810,1.1810,1.1810,1.1810, 0.8338,0.8338,0.9431,1.1868,1.1739,1.3830,1.3880,1.3542,1.1758,1.1630,1.1630,1.1630,1.1630, 0.8252,0.8252,0.9319,1.1850,1.1667,1.3752,1.3757,1.3375,1.1575,1.1445,1.1445,1.1445,1.1445, 0.8161,0.8161,0.9196,1.1813,1.1583,1.3672,1.3621,1.3201,1.1391,1.1256,1.1256,1.1256,1.1256, 0.8052,0.8052,0.9070,1.1772,1.1480,1.3590,1.3473,1.3019,1.1211,1.1062,1.1062,1.1062,1.1062, 0.7722,0.7722,0.8740,1.1442,1.1150,1.3260,1.3143,1.2689,1.0881,1.0663,1.0663,1.0663,1.0663, 0.5882,0.5882,0.6900,0.9602,0.9310,1.1420,1.1303,1.0849,0.9041,0.8997,0.8997,0.8997,0.8997, 0.3942,0.3942,0.4960,0.7662,0.7370,0.9480,0.9363,0.8909,0.7101,0.6985,0.6985,0.6985,0.6985, 0.2022,0.2022,0.3040,0.5742,0.5450,0.7560,0.7443,0.6989,0.5181,0.5015,0.5015,0.5015,0.5015 ) \begintext Normal force coefficients as function of the angle-of-attack and flow regime (i.e., Mach Number) \begindata HUY_CN=( 0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000,0.0000, 0.0034,0.0034,0.0032,0.0027,0.0025,0.0027,0.0031,0.0034,0.0042,0.0046,0.0046,0.0046,0.0046, 0.0069,0.0069,0.0063,0.0055,0.005, 0.0055,0.0065,0.0070,0.0085,0.0093,0.0093,0.0093,0.0093, 0.0105,0.0105,0.0095,0.0085,0.0075,0.0086,0.0102,0.0109,0.0128,0.0141,0.0141,0.0141,0.0141, 0.0140,0.0140,0.0129,0.0116,0.0103,0.0121,0.0141,0.0149,0.0172,0.0190,0.0190,0.0190,0.0190, 0.0176,0.0176,0.0168,0.0148,0.0134,0.0158,0.0181,0.0191,0.0216,0.0240,0.0240,0.0240,0.0240, 0.0212,0.0212,0.0210,0.0184,0.0169,0.0197,0.0221,0.0233,0.0262,0.0296,0.0296,0.0296,0.0296, 0.0248,0.0248,0.0251,0.0224,0.0207,0.0236,0.0261,0.0275,0.0309,0.0359,0.0359,0.0359,0.0359, 0.0287,0.0287,0.0292,0.0267,0.0246,0.0276,0.0301,0.0316,0.0357,0.0426,0.0426,0.0426,0.0426, 0.0327,0.0327,0.0335,0.031, 0.0286,0.0315,0.0340,0.0357,0.0407,0.0495,0.0495,0.0495,0.0495, 0.0367,0.0367,0.0379,0.0351,0.0325,0.0355,0.0380,0.0398,0.0460,0.0565,0.0565,0.0565,0.0565, 0.0406,0.0406,0.0424,0.0392,0.0364,0.0394,0.0418,0.0438,0.0516,0.0633,0.0633,0.0633,0.0633, 0.0448,0.0448,0.0471,0.0435,0.0402,0.0433,0.0457,0.0478,0.0574,0.0698,0.0698,0.0698,0.0698, 0.0490,0.0490,0.0518,0.0478,0.0439,0.0471,0.0496,0.0518,0.0634,0.0767,0.0767,0.0767,0.0767, 0.0533,0.0533,0.0561,0.0519,0.0476,0.0509,0.0534,0.0558,0.0696,0.0838,0.0838,0.0838,0.0838, 0.0576,0.0576,0.0608,0.0561,0.0513,0.0546,0.0572,0.0599,0.0756,0.0909,0.0909,0.0909,0.0909, 0.0618,0.0618,0.0656,0.0602,0.0550,0.0582,0.0610,0.0640,0.0816,0.0979,0.0979,0.0979,0.0979, 0.0661,0.0661,0.0701,0.0642,0.0586,0.0618,0.0648,0.0681,0.0875,0.1047,0.1047,0.1047,0.1047, 0.0704,0.0704,0.0743,0.0682,0.0621,0.0653,0.0686,0.0722,0.0936,0.1114,0.1114,0.1114,0.1114, 0.0747,0.0747,0.0785,0.0721,0.0657,0.0689,0.0724,0.0765,0.0999,0.1178,0.1178,0.1178,0.1178, 0.0787,0.0787,0.0827,0.0760,0.0691,0.0726,0.0762,0.0807,0.1059,0.1236,0.1236,0.1236,0.1236, 0.0826,0.0826,0.0868,0.0800,0.0726,0.0761,0.0800,0.0849,0.1116,0.1295,0.1295,0.1295,0.1295, 0.0863,0.0863,0.0907,0.0837,0.0760,0.0797,0.0838,0.0892,0.1172,0.1359,0.1359,0.1359,0.1359, 0.0902,0.0902,0.0949,0.0874,0.0794,0.0832,0.0877,0.0936,0.1228,0.1420,0.1420,0.1420,0.1420, 0.0939,0.0939,0.0991,0.0912,0.0828,0.0868,0.0917,0.0981,0.1282,0.1478,0.1478,0.1478,0.1478, 0.0974,0.0974,0.1030,0.0950,0.0861,0.0903,0.0957,0.1028,0.1334,0.1532,0.1532,0.1532,0.1532, 0.1009,0.1009,0.1069,0.0986,0.0894,0.0939,0.0997,0.1075,0.1384,0.1582,0.1582,0.1582,0.1582, 0.1044,0.1044,0.1110,0.1024,0.0927,0.0975,0.1039,0.1125,0.1431,0.1628,0.1628,0.1628,0.1628, 0.1081,0.1081,0.1153,0.1062,0.0962,0.1013,0.1082,0.1177,0.1475,0.1669,0.1669,0.1669,0.1669, 0.1161,0.1161,0.1233,0.1142,0.1042,0.1093,0.1162,0.1257,0.1555,0.1749,0.1749,0.1749,0.1749, 0.1411,0.1411,0.1483,0.1392,0.1292,0.1343,0.1412,0.1507,0.1805,0.1999,0.1999,0.1999,0.1999, 0.1411,0.1411,0.1483,0.1392,0.1292,0.1343,0.1412,0.1507,0.1805,0.1999,0.1999,0.1999,0.1999, 0.1211,0.1211,0.1283,0.1192,0.1092,0.1143,0.1212,0.1307,0.1605,0.1799,0.1799,0.1799,0.1799 ) \begintext Number of aerodynamic regimes and angle of attacks considered. \begindata HUY_AOA_Nr=(33) HUY_Reg_Nr=(13)