📄 interpolation_data.m
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% Interpolation data for aerodynamic calculation model
% LiuXiangChun
% The college of astronautics NWPU
% Date:2007-06-07
disp('Loading data from file Interpolation_data.m ...')
%**************************************************************************
% 2--Interpolation Table data
%**************************************************************************
% 2.1--Cy
%========================================================================================================================================================================================================================================================
% 2.1.1--Cywing_Table data
%========================================================================================================================================================================================================================================================
% Tnterpolation data of Cywing
%---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------
Cywing_input1=[0.25 0.50 1.0 1.5];
Cywing_input2=[-3.5 -3.0 -2.5 -2.0 -1.5 -1.0 -0.5 0.0 0.25 0.50 0.75 1.0 1.5 2.0 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0 6.5 7.0 7.5 8.0 8.5 9.0 10.0 11.0 12.0];
Cywing_input3=[0.0 1.0 2.0 3.0];
Cywing_Table(:,:,1)=[.0180 .0191 .0202 .0220 .0238 .0255 .0280 .0307 .0327 .0337 .0339 .0331 .0300 .0264 .0226 .0198 .0175 .0155 .0150 .0137 .0125 .0114 .0106 .0099 .0092 .0086 .0080 .0076 .0071 .0068 .0067
.0175 .0186 .0200 .0216 .0235 .0245 .0273 .0308 .0315 .0317 .0313 .0305 .0281 .0252 .0221 .0198 .0174 .0154 .0147 .0134 .0122 .0112 .0105 .0098 .0090 .0085 .0079 .0076 .0071 .0068 .0067
.0166 .0175 .0182 .0195 .0210 .0225 .0265 .0282 .0280 .0274 .0269 .0262 .0246 .0227 .0208 .0192 .0173 .0153 .0140 .0128 .0117 .0108 .0100 .0094 .0088 .0083 .0078 .0075 .0070 .0068 .0067
.0160 .0162 .0163 .0172 .0182 .0196 .0220 .0244 .0239 .0233 .0228 .0223 .0212 .0199 .0186 .0174 .0161 .0148 .0135 .0124 .0112 .0103 .0097 .0092 .0086 .0080 .0076 .0074 .0069 .0068 .0067];
Cywing_Table(:,:,2)=[.0175 .0193 .0205 .0225 .0240 .0280 .0285 .0296 .0310 .0316 .0316 .0309 .0281 .0253 .0225 .0200 .0185 .0164 .0152 .0138 .0125 .0115 .0107 .0099 .0091 .0084 .0080 .0074 .0066 .0060 .0058
.0174 .0185 .0198 .0215 .0234 .0243 .0283 .0296 .0300 .0300 .0296 .0289 .0264 .0237 .0214 .0190 .0173 .0155 .0148 .0136 .0123 .0113 .0105 .0098 .0090 .0084 .0080 .0074 .0066 .0060 .0058
.0165 .0173 .0180 .0193 .0208 .0223 .0264 .0269 .0266 .0260 .0254 .0247 .0230 .0226 .0200 .0183 .0169 .0152 .0136 .0124 .0114 .0106 .0099 .0092 .0086 .0082 .0076 .0072 .0065 .0060 .0058
.0157 .0160 .0162 .0170 .0180 .0193 .0218 .0232 .0228 .0223 .0218 .0213 .0202 .0191 .0179 .0168 .0156 .0144 .0128 .0120 .0111 .0100 .0093 .0087 .0083 .0077 .0073 .0066 .0065 .0060 .0058];
Cywing_Table(:,:,3)=[.0170 .0172 .0203 .0223 .0242 .0270 .0280 .0270 .0282 .0288 .0291 .0288 .0262 .0239 .0213 .0193 .0175 .0163 .0156 .0141 .0128 .0118 .0110 .0101 .0094 .0088 .0082 .0077 .0070 .0066 .0064
.0172 .0183 .0196 .0213 .0235 .0259 .0270 .0267 .0272 .0274 .0270 .0264 .0244 .0222 .0204 .0186 .0164 .0155 .0152 .0137 .0124 .0115 .0107 .0099 .0092 .0086 .0082 .0077 .0070 .0066 .0064
.0165 .0172 .0178 .0191 .0207 .0225 .0245 .0246 .0244 .0241 .0237 .0230 .0216 .0201 .0186 .0172 .0160 .0148 .0142 .0130 .0120 .0110 .0102 .0093 .0088 .0082 .0078 .0074 .0068 .0064 .0062
.0156 .0159 .0161 .0170 .0185 .0195 .0209 .0217 .0214 .0210 .0206 .0202 .0192 .0181 .0170 .0160 .0150 .0140 .0134 .0128 .0117 .0106 .0098 .0090 .0086 .0080 .0076 .0072 .0066 .0062 .0060];
Cywing_Table(:,:,4)=[.0169 .0171 .0202 .0230 .0234 .0255 .0250 .0234 .0244 .0252 .0254 .0252 .0232 .0212 .0193 .0180 .0168 .0157 .0142 .0130 .0120 .0110 .0106 .0102 .0098 .0092 .0088 .0084 .0078 .0070 .0062
.0171 .0182 .0195 .0212 .0232 .0238 .0268 .0230 .0236 .0238 .0238 .0233 .0218 .0202 .0188 .0184 .0162 .0150 .0138 .0126 .0117 .0108 .0105 .0101 .0096 .0088 .0083 .0078 .0070 .0065 .0062
.0163 .0170 .0176 .0189 .0209 .0210 .0216 .0218 .0220 .0219 .0216 .0211 .0199 .0186 .0174 .0163 .0152 .0143 .0134 .0123 .0114 .0106 .0104 .0100 .0092 .0086 .0080 .0076 .0068 .0064 .0062
.0155 .0157 .0159 .0169 .0183 .0192 .0199 .0200 .0198 .0197 .0195 .0190 .0180 .0171 .0161 .0152 .0144 .0136 .0128 .0120 .0112 .0105 .0102 .0098 .0088 .0084 .0078 .0074 .0066 .0063 .0062];
%----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------
%========================================================================================================================================================================================================================================================
% Cywing data end
%========================================================================================================================================================================================================================================================
%=====================================================================================================================
% 2.1.2--Cybody data
%=====================================================================================================================
%-------------------------------------------------------------------
% 2.1.2.1--Interpolation data of Cy1n(锥头体圆柱段法向力系数插值表数据)
%---------------------------------------------------------------------------------------------------------------------
Cy1n_Row=[0.0 0.5 1.0 2.0 3.0 4.0];
Cy1n_Column=[-0.5 -0.4 -0.3 -0.2 -0.1 0.0 0.2 0.3 0.4 0.6 0.8 1.0 1.2 1.4 1.6];
Cy1n_Table=[.0350 .0350 .0350 .0350 .0350 .0350 .0350 .0348 .0345 .0338 .0335 .0330 .0325 .0321 .0318
.0350 .0360 .0370 .0380 .0390 .0400 .0446 .0463 .0475 .0476 .0470 .0459 .0443 .0430 .0420
.0350 .0360 .0371 .0381 .0392 .0402 .0450 .0474 .0489 .0519 .0522 .0520 .0514 .0500 .0490
.0350 .0361 .0371 .0382 .0392 .0403 .0453 .0476 .0490 .0530 .0550 .0561 .0560 .0558 .0554
.0350 .0361 .0372 .0382 .0393 .0404 .0455 .0478 .0495 .0531 .0555 .0565 .0576 .0580 .0582
.0350 .0361 .0372 .0383 .0394 .0405 .0456 .0479 .0500 .0532 .0558 .0574 .0585 .0590 .0593 ];
%---------------------------------------------------------------------------------------------------------------------
% 2.1.2.2--Interpolation data of Cy1t(锥形收缩尾部法向力系数插值表数据)
%==============================================================================================
% M<=1
%-----------------------------------------------------------
Cy1t_Row1=[-1.0 -.75 -.65 -.5 -.41 -.25 -.1 0.0];
Cy1t_Table1=[-1.32 -2.0 -2.5 -3.38 -3.5 -3.6 -3.5 -3.4];
%-----------------------------------------------------------
% M>1
%-------------------------------------------------------------------------
Cy1t_Row2=[0 .25 .5 .75 1.0 1.25 1.5 1.75 2.0 2.25 2.5];
Cy1t_Table2=[0 -.5 -.86 -1.2 -1.44 -1.65 -1.8 -1.91 -1.96 -2.0 -2.0];
%-------------------------------------------------------------------------
%==============================================================================================
% 2.1.2.3--Interpolation data of Cy1v(B)(粘性法向力系数插值表数据)
%===========================================================================================
% F1
%----------------------------------------
F1_Row=[2 4 6 8];
F1_Column=[8 10 12 14];
F1_Table=[7.1 9.45 11.8 14.25
6.2 8.50 10.9 13.25
5.2 7.45 9.80 12.1
4.0 6.20 8.6 11.0 ];
%----------------------------------------
% F2
%---------------------------------------------------------------------------
F2_Row=[0 5 10 15 20 25];
F2_Column=[1.0 1.5 2.0 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0 7.0];
F2_Table=[0.14 0.18 0.24 0.31 0.40 0.50 0.62 0.77 0.90 0.97 0.99 0.94
0.43 0.47 0.55 0.64 0.74 0.87 0.96 1.03 1.05 1.03 0.99 0.94
0.76 0.80 0.87 0.98 1.09 1.15 1.16 1.13 1.07 1.03 0.99 0.94
1.32 1.35 1.37 1.37 1.35 1.29 1.18 1.10 1.05 1.03 0.99 0.94
1.87 1.84 1.78 1.68 1.44 1.26 1.16 1.10 1.05 1.03 0.99 0.94
1.94 1.87 1.77 1.64 1.40 1.24 1.15 1.09 1.05 1.03 0.99 0.94];
%---------------------------------------------------------------------------
%===========================================================================================
%=====================================================================================================================
% Cybody data end
%=====================================================================================================================
%==========================================================================
% 2.1.3--干扰因子
%==========================================================================
% 2.1.3.1--Interpolation data of Kaa(干扰因子Kaa插值表数据)
%===================================================================
% K_bw("aa"情况下弹翼对弹体的干扰因子) (p103 f2-1-43)
%----------------------------------------------------------------
D_L=[0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0];
K_bw_Table=[0.0 0.13 0.38 0.43 0.6 0.8 1.0 1.22 1.46 1.73 2.0];
%----------------------------------------------------------------
% K_wb("aa"情况下弹体对外露翼的干扰因子)
%----------------------------------------------------------------
% D/L;
K_wb_Table=[1.0 1.08 1.16 1.25 1.34 1.44 1.55 1.66 1.76 1.88 2.0];
%----------------------------------------------------------------
% k_wb("b0"情况下弹体对外露翼的干扰因子)
%----------------------------------------------------------------
% D/L;
k_wb_Table=[1.0 0.97 0.95 0.94 0.935 0.94 0.945 0.955 0.97 0.98 1.0];
%----------------------------------------------------------------
% k_bw("b0"情况下弹翼对弹体的干扰因子)
%----------------------------------------------------------------
% D/L;
k_bw_Table=[0.0 0.1 0.2 0.3 0.41 0.51 0.6 0.7 0.8 0.9 1.0];
%----------------------------------------------------------------
% K_press(p106 f2-1-47)
%----------------------------------------------------------------
Msina=[0.0 0.38 0.4 0.5 0.6 0.7 0.8 1.0 1.2];
K_press_Table=[1.0 1.0 0.95 0.5 0.32 0.24 0.2 0.16 0.16];
%===================================================================
% 2.2.3.2--Interpolation data of i(干扰因子i插值表数据)
%=========================================================================
% Interpolation data of Cy_wv(干扰因子i插值表数据)
%========================================================================
% Xs_R p106 f2-1-48
%--------------------------------------------------------
Xs_R_input1=[1 2]; % 1表示层流；2表示紊流
Xs_R_input2=[5 7.5 10 12.5 15 17.5 20 25 30];
Xs_R_Table=[4.0 3.5 3.0 2.35 2.0 1.7 1.42 1.05 0.8
2.88 1.78 1.23 1.0 0.85 0.73 0.63 0.5 0.43];
%--------------------------------------------------------
% Ctao_a p106 f2-1-49
%--------------------------------------------------------
Ctao_a_input=[0.5 3 5 7];
Ctao_a_Table=[0.51 1.0 1.5 2.0];
%--------------------------------------------------------
% Yv_R p113 f2-1-62
%--------------------------------------------------------
Yv_R_input=[0 1 2 3 4 5 6 6.5];
Yv_R_Table=[0.91 1.26 1.53 1.74 1.9 2.03 2.14 2.17];
%--------------------------------------------------------
% Zv_R p113 f2-1-62
%--------------------------------------------------------
Zv_R_input=[0 1 2 3 4 5 6 6.5];
Zv_R_Table=[0.48 0.62 0.7 0.75 0.76 0.78 0.79 0.78];
%--------------------------------------------------------
% i_body 附图2-1-50至2-1-61 p107-112 三角形翼
%--------------------------------------------------------
i_body_input1=[0 0.4 0.8 1.2 1.6]; % 2Yv/L_wing
i_body_input2=[0 0.4 0.8 1.2 1.6 2.0 2.4 2.8]; % 2Zv/L_wing
i_body_input3=[0 0.2 0.4 0.6]; % D/L_wing
% i_body
i_body_Table(:,:,1)=-[0 3.0 3.5 2.0 1.4 1.1 0.88 0.75
0 1.3 1.9 1.7 1.3 1.0 0.85 0.73
0 0.65 1.1 1.15 1.05 0.9 0.78 0.65
0 0.4 0.68 0.77 0.8 0.74 0.66 0.6
0 0.25 0.45 0.67 0.7 0.68 0.62 0.57];
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