📄 interpolation_data.m
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i_body_Table(:,:,2)=-[0 2.5 3.8 2.0 1.45 1.12 0.9 0.77
0 1.2 1.85 1.7 1.4 1.05 0.88 0.75
0 0.68 1.2 1.2 1.1 0.95 0.8 0.72
0 0.4 0.67 0.78 0.79 0.76 0.7 0.65
0 0.25 0.47 0.58 0.63 0.62 0.60 0.57];
i_body_Table(:,:,3)=-[0 0.6 3.8 1.93 1.32 0.97 0.75 0.65
0 0.6 1.5 1.5 1.2 0.92 0.78 0.6
0 0.4 0.85 1.0 0.93 0.8 0.66 0.58
0 0.28 0.5 0.6 0.65 0.6 0.57 0.5
0 0.17 0.32 0.42 0.48 0.49 0.48 0.46];
i_body_Table(:,:,4)=-[0 0.0 3.2 1.7 1.0 0.77 0.62 0.56
0 0.0 0.95 1.2 0.9 0.72 0.59 0.57
0 0.1 0.53 0.7 0.68 0.61 0.53 0.45
0 0.15 0.35 0.48 0.52 0.5 0.46 0.43
0 0.15 0.25 0.35 0.39 0.4 0.39 0.38];
%--------------------------------------------------------
%========================================================================
% i_tail 附图2-1-50至2-1-61 p107-112
%--------------------------------------------------------------------------
i_tail_input1=i_body_input1; % 2Yv/L_tail
i_tail_input2=i_body_input2; % 2Zv/L_tail
i_tail_input3=i_body_input3; % D/L_tail
i_tail_Table=i_body_Table; % i_tail
%--------------------------------------------------------------------------
%=========================================================================
%==========================================================================
% 干扰因子 end
%==========================================================================
% 2.2--Cx
%========================================================================================================================================================================================================================================================
% 2.2.1--Cx_wing_Table data
%========================================================================================================================================================================================================================================================
% 2.2.1.1--Cx0_wing
%===========================================================================
% Tnterpolation data of Cx0_wing
%--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------
% C1 page77 figure2-1-9 (用于判断是否为大展弦比翼page48)
figure219_input=[0 0.1 0.2 0.3 0.4 0.5 0.7 1.0];
figure219_Table=[0 0.25 0.45 0.49 0.47 0.4 0.2 0];
% eta_t page136
figure221_input1=[0.0 0.2 0.4]; %转捩点的相对位置
figure221_input2=[0.00 0.02 0.04 0.06 0.08 0.10 0.12]; %翼型相对厚度
figure221_Table=[1.00 1.05 1.105 1.16 1.22 1.29 1.36
1.00 1.035 1.08 1.125 1.175 1.23 1.285
1.00 1.025 1.05 1.08 1.12 1.15 1.18]; %修正系数
% (Cf)_m=0 page137
figure222_input1=[0 0.1 0.2 0.3 0.4 0.5 0.6 1.0];
figure222_input2=[1.0E6 1.5E6 2.0E6 3.0E6 4.0E6 5.0E6 6.0E6 7.0E6 8.0E6 9.0E6 1.0E7 1.5E7 2.0E7 3.0E7 4.0E7 5.0E7 6.0E7 7.0E7 8.0E7 9.0E7 1.0E8 1.5E8 2.0E8 3.0E8];
figure222_Table=[0.0090 0.0083 0.0079 0.0073 0.0070 0.0067 0.0065 0.0063 0.0062 0.0061 0.0060 0.0056 0.0054 0.0050 0.0048 0.0046 0.0045 0.0044 0.0043 0.0042 0.0041 0.0040 0.0038 0.0036
0.0085 0.0078 0.0075 0.0069 0.0066 0.0063 0.0061 0.0060 0.0058 0.0057 0.0056 0.0053 0.0050 0.0047 0.0045 0.0043 0.0042 0.0041 0.0040 0.0039 0.0038 0.0036 0.0035 0.0033
0.0080 0.0074 0.0070 0.0065 0.0060 0.0058 0.0056 0.0055 0.0053 0.0052 0.0051 0.0048 0.0046 0.0043 0.0041 0.0040 0.0039 0.0038 0.0037 0.0036 0.0035 0.0034 0.0032 0.0030
0.0075 0.0068 0.0065 0.0059 0.0055 0.0053 0.0051 0.0050 0.0048 0.0047 0.0046 0.0043 0.0041 0.0038 0.0037 0.0036 0.0035 0.0034 0.0033 0.0032 0.0031 0.0030 0.0029 0.0027
0.0069 0.0062 0.0058 0.0054 0.0050 0.0048 0.0046 0.0044 0.0043 0.0042 0.0041 0.0038 0.0036 0.0034 0.0032 0.0031 0.0030 0.0029 0.0028 0.0027 0.0026 0.0026 0.0025 0.0024
0.0063 0.0056 0.0052 0.0048 0.0045 0.0042 0.0040 0.0039 0.0038 0.0037 0.0036 0.0034 0.0031 0.0029 0.0027 0.0026 0.0025 0.0025 0.0024 0.0024 0.0023 0.0022 0.0021 0.0020
0.0057 0.0051 0.0047 0.0042 0.0039 0.0037 0.0035 0.0034 0.0033 0.0032 0.0031 0.0028 0.0026 0.0024 0.0023 0.0022 0.0021 0.0021 0.0020 0.0020 0.0019 0.0018 0.0017 0.0016
0.0027 0.0018 0.0015 0.0013 0.0012 0.0011 0.0010 0.0009 0.0008 0.0007 0.0006 0.0005 0.0005 0.0004 0.0004 0.0004 0.0003 0.0003 0.0003 0.0002 0.0002 0.0001 0.0001 0.0000];
% eta_M page139
figure224_input1=[0.0 0.5 0.8 1.0];
figure224_input2=[0.0 0.5 1 2 3 4 5 6];
figure224_Table=[1.0 0.97 0.915 0.75 0.62 0.51 0.42 0.35;1.0 0.975 0.93 0.795 0.66 0.568 0.49 0.43;1.0 0.98 0.945 0.835 0.73 0.645 0.57 0.518;1.0 0.992 0.98 0.965 0.94 0.908 0.86 0.80];
% phi page147
figure2212_input=[0.000 0.500 1.000 1.500 2.000 2.500 3.000 3.500 4.000 4.500 5.000 5.500 6.000 6.500];
figure2212_Table=[0.000 0.045 0.115 0.215 0.340 0.455 0.557 0.645 0.720 0.783 0.840 0.880 0.910 0.930];
% Cxp page144-146
figure229_input1=[1.00 2.00 3.00 4.00];
figure229_input2=[0.00 0.15 0.25 0.36 0.50 1.00 1.50 2.00 2.50 3.00 3.50 4.00 4.50 5.00 5.50 6.00 6.50 7.00 10.0 12.0 15.0];
figure229_input3=[0.0 0.2 1.0];
figure229_Table(:,:,3)=[1.530 1.630 1.680 1.750 1.870 2.080 2.010 1.738 1.460 1.230 1.060 0.940 0.840 0.760 0.680 0.620 0.570 0.540 0.435 0.380 0.300
0.870 0.910 0.930 0.960 0.990 1.148 1.380 1.500 1.500 1.390 1.230 1.021 0.900 0.810 0.715 0.650 0.600 0.560 0.435 0.380 0.300
0.450 0.470 0.480 0.500 0.520 0.610 0.730 0.870 1.050 1.190 1.210 1.130 1.000 0.890 0.785 0.705 0.640 0.580 0.460 0.380 0.300
0.220 0.230 0.240 0.250 0.260 0.300 0.380 0.460 0.570 0.705 0.825 0.925 0.980 0.960 0.808 0.780 0.650 0.628 0.485 0.410 0.300];
figure229_Table(:,:,2)=[1.810 1.890 1.930 1.960 1.990 1.990 1.840 1.620 1.400 1.200 1.060 0.940 0.840 0.744 0.680 0.610 0.570 0.530 0.420 0.360 0.260
0.960 1.120 1.140 1.190 1.220 1.360 1.460 1.460 1.400 1.270 1.140 1.020 0.908 0.820 0.732 0.655 0.600 0.540 0.420 0.360 0.260
0.600 0.630 0.640 0.670 0.680 0.782 0.890 1.000 1.060 1.100 1.090 1.030 0.970 0.880 0.810 0.705 0.640 0.600 0.430 0.360 0.260
0.320 0.330 0.340 0.360 0.370 0.430 0.480 0.560 0.640 0.790 0.800 0.850 0.880 0.880 0.850 0.800 0.720 0.590 0.450 0.370 0.260];
figure229_Table(:,:,1)=[1.920 1.920 1.920 1.920 1.910 1.840 1.740 1.560 1.390 1.210 1.080 0.960 0.860 0.780 0.700 0.650 0.580 0.540 0.420 0.350 0.250
1.300 1.320 1.340 1.350 1.360 1.380 1.370 1.310 1.240 1.170 1.080 1.000 0.900 0.800 0.720 0.650 0.600 0.560 0.420 0.350 0.250
0.800 0.810 0.820 0.830 0.840 0.890 0.930 0.960 0.990 1.000 0.980 0.940 0.890 0.820 0.760 0.700 0.640 0.600 0.430 0.350 0.250
0.460 0.465 0.465 0.470 0.480 0.520 0.540 0.570 0.610 0.650 0.700 0.720 0.750 0.760 0.750 0.735 0.700 0.630 0.430 0.360 0.250];
%--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------
%========================================================================================================================================================================================================================================================
% Cx_wing_Table data end
%========================================================================================================================================================================================================================================================
%========================================================================================================================================================================================================================================================
% 2.2.2--Cx_body_Table data
%========================================================================================================================================================================================================================================================
% Tnterpolation data of Cx0_body 锥形头部
%--------------------------------------------------------------------------------------------------------------
% Cxn 头部阻力系数 page149
figure2216_input1=[2.00 3.00 4.00 5.00];
figure2216_input2=[0.00 0.50 0.83 1.00 1.25 1.50 2.00 2.50 3.00 3.50 4.00 4.50 5.00];
figure2216_Table=[-0.005 -0.004 0.010 0.100 0.190 0.200 0.182 0.168 0.156 0.149 0.144 0.138 0.135
-0.005 -0.004 0.010 0.060 0.120 0.115 0.100 0.090 0.082 0.078 0.074 0.071 0.069
-0.005 -0.004 0.010 0.040 0.078 0.072 0.061 0.055 0.051 0.047 0.045 0.044 0.042
-0.005 -0.004 0.010 0.028 0.055 0.050 0.044 0.039 0.037 0.034 0.032 0.031 0.030];
% Cxt 尾部阻力系数 page164-166 Subsonic & Transonic
figure2232_input1=[3 5 10];
figure2232_input2=[0.3 0.5 0.8 0.9 0.95 1.0 1.1 1.2 1.5];
figure2232_input3=[0.6 0.8 1.0];
figure2232_Table(:,:,1)=[0.01 0.011 0.014 0.017 0.028 0.026 0.011 0.012 0.011
0.02 0.022 0.026 0.031 0.057 0.056 0.035 0.031 0.03
0.045 0.049 0.06 0.115 0.150 0.150 0.116 0.110 0.077];
figure2232_Table(:,:,2)=[0.014 0.016 0.018 0.02 0.025 0.03 0.014 0.017 0.012
0.022 0.025 0.03 0.038 0.06 0.064 0.04 0.04 0.027
0.05 0.05 0.073 0.014 0.0175 0.18 0.14 0.128 0.092];
figure2232_Table(:,:,3)=[0.015 0.016 0.017 0.019 0.025 0.032 0.017 0.02 0.013
0.026 0.028 0.032 0.04 0.06 0.064 0.042 0.044 0.032
0.042 0.047 0.062 0.10 0.18 0.194 0.145 0.14 0.097];
% Cxt 尾部阻力系数 page167 Supersonic
figure2235_input1=[0.25 0.4 0.5 0.8];
figure2235_input2=[0.1 0.3 0.5 1.0 1.5 2.5 3.5 4.5 5.5 6.5 7.5];
figure2235_Table=[1.78 1.1 0.84 0.48 0.29 0.14 0.08 0.052 0.035 0.025 0.020
1.1 0.67 0.50 0.30 0.19 0.095 0.056 0.0375 0.027 0.020 0.015
0.7 0.44 0.33 0.20 0.13 0.072 0.043 0.030 0.021 0.015 0.012
0.13 0.07 0.05 0.035 0.032 0.012 0.009 0.007 0.005 0.004 0.003];
% Cxb 底部阻力系数
% Cxb1 page170
figure2239_input1=[0.00 0.10];
figure2239_input2=[0.40 0.60 0.80 0.92 1.00 1.05 1.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00 3.20 3.40 3.60 3.80 4.00 4.20 4.40 4.60 4.80 5.00 6.00 7.00 8.00 9.00 10.00];
figure2239_Table=[0.13 0.12 0.12 0.140 0.194 0.198 0.194 0.186 0.175 0.163 0.151 0.139 0.127 0.115 0.103 0.095 0.087 0.081 0.075 0.070 0.065 0.060 0.058 0.053 0.050 0.047 0.036 0.030 0.024 0.021 0.020
0.13 0.12 0.12 0.168 0.287 0.283 0.273 0.267 0.265 0.229 0.194 0.167 0.145 0.129 0.115 0.104 0.094 0.085 0.078 0.072 0.065 0.060 0.058 0.053 0.050 0.047 0.036 0.030 0.024 0.021 0.020];
% Cxb2 page170-171
figure2240_input1=[0.8 0.9 1.0 1.1 1.2 1.3 1.4];
figure2240_input2=[0 1 1.5 2 3 4 5 6 7 8 9 10];
figure2240_Table=[0 0.195 0.23 0.23 0.172 0.135 0.124 0.12 0.1 0.074 0.04 0.008
0 0.252 0.275 0.246 0.18 0.16 0.146 0.125 0.1 0.075 0.05 0.02
0 0.24 0.28 0.03 0.031 0.292 0.266 0.24 0.21 0.18 0.155 0.13
0 0.126 0.16 0.193 0.22 0.214 0.2 0.177 0.16 0.14 0.125 0.11
0 0.14 0.17 0.188 0.2 0.195 0.185 0.168 0.15 0.134 0.11 0.105
0 0.1 0.135 0.16 0.185 0.19 0.186 0.172 0.16 0.14 0.125 0.11
0 0.075 0.1 0.124 0.16 0.18 0.19 0.188 0.174 0.155 0.13 0.105];
%--------------------------------------------------------------------------------------------------------------
%========================================================================================================================================================================================================================================================
% Cx_body_Table data end
%========================================================================================================================================================================================================================================================
% 2.2.3--Cxi_MaoWing page180-181 figure2-2-54至2-2-57
%--------------------------------------------------------------------------
figure2254_input1=[0 10 20 30 40 50 55 60 65 70 75];% sweepback_0前缘后掠角
figure2254_input2=[1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0];% AspectRatio 展弦比
figure2254_input3=[0.2 0.5 0.7 1.0]; % Eta 梢根比
figure2254_Table(:,:,1)=[1 1 1 1 1 1 1 1
1 1 1 1 1 1 1 1
1 1 1 1 1 1 1 1
1 1 1 1 1 1 1 1
1.00 1.00 1.00 1.00 1.002 1.002 1.003 1.003
1.00 1.00 1.002 1.005 1.007 1.01 1.012 1.013
1.00 1.001 1.005 1.011 1.016 1.02 1.025 1.027
1.00 1.003 1.013 1.024 1.033 1.04 1.047 1.05
1.00 1.006 1.024 1.045 1.064 1.08 1.088 1.092
1.00 1.017 1.05 1.095 1.13 1.17 1.20 1.22
1.002 1.045 1.12 1.21 1.28 1.34 1.39 1.43
];
figure2254_Table(:,:,2)=[1 1 1 1 1 1 1 1
1 1 1 1 1 1 1 1
1.00 1.00 1.00 1.001 1.004 1.007 1.009 1.012
1.00 1.00 1.002 1.006 1.011 1.015 1.02 1.025
1.00 1.002 1.008 1.015 1.023 1.31 1.04 1.05
1.00 1.005 1.016 1.03 1.048 1.063 1.07 1.094
1.00 1.008 1.024 1.047 1.07 1.09 1.113 1.134
1.001 1.014 1.036 1.07 1.10 1.135 1.166 1.19
1.003 1.022 1.06 1.113 1.16 1.21 1.26 1.31
1.005 1.042 1.10 1.19 1.30 1.40 1.55 1.70
1.013 1.085 1.20 1.36 1.55 1.72 1.9 2.2
];
figure2254_Table(:,:,3)=[1 1 1 1 1 1 1 1
1.00 1.00 1.00 1.003 1.007 1.01 1.015 1.018
1.00 1.00 1.003 1.007 1.013 1.02 1.026 1.033
1.00 1.002 1.007 1.015 1.025 1.035 1.045 1.056
1.00 1.005 1.015 1.028 1.044 1.06 1.076 1.093
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