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📄 interpolation_data.m

📁 本程序的开发环境为MATLAB6.5版本
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                         1.001 1.010 1.025 1.05  1.08  1.104 1.13  1.155
                         1.002 1.015 1.037 1.07  1.107 1.14  1.17  1.20
                         1.003 1.02  1.05  1.1   1.15  1.195 1.23  1.28
                         1.006 1.035 1.08  1.15  1.22  1.28  1.34  1.41
                         1.01  1.057 1.14  1.24  1.34  1.43  1.52  1.62
                         1.02  1.11  1.25  1.4   1.55  1.69  1.83  1.98              
                        ];
figure2254_Table(:,:,4)=[1.00  1.00  1.002 1.006 1.012 1.018 1.025 1.03
                         1.00  1.002 1.005 1.011 1.02  1.03  1.04  1.05
                         1.001 1.003 1.008 1.019 1.031 1.045 1.06  1.073
                         1.001 1.006 1.015 1.03  1.05  1.07  1.09  1.108
                         1.002 1.010 1.025 1.047 1.074 1.103 1.13  1.155
                         1.004 1.017 1.043 1.078 1.117 1.16  1.2   1.238
                         1.005 1.023 1.058 1.10  1.15  1.206 1.26  1.32
                         1.007 1.033 1.08  1.136 1.2   1.27  1.35  1.43
                         1.012 1.048 1.11  1.19  1.29  1.4   1.5   1.61
                         1.017 1.075 1.18  1.293 1.42  1.56  1.69  1.83
                         1.03  1.13  1.29  1.45  1.63  1.82  2.0   2.2                         
                        ];
                        
% page 182 figure 2-2-58
figure2258_input1=[3 4 5 6];
figure2258_input2=[0.2667 0.4 0.6 0.8 0.9 1.0];
figure2258_Table=[0.70  0.66  0.565 0.40  0.24  0.0
                  0.77  0.73  0.63  0.45  0.28  0.0
                  0.85  0.80  0.68  0.50  0.325 0.0
                  0.91  0.85  0.725 0.535 0.355 0.0
                 ];
                 
% page 183 figure 2-2-59
figure2259_input1=[0 1];
figure2259_input2=[0.0  0.10  0.20  0.30  0.40  0.50  0.60];
figure2259_Table=[0.61  0.38  0.25  0.175 0.125 0.08  0.06
                  0.80  0.72  0.605 0.47  0.315 0.20  0.14
                 ];
%--------------------------------------------------------------------------
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
% 2.3--Xd

%--------------------------------------------------------------------------
% Tnterpolation Table data 
%--------------------------------------------------------------------------

% page70 K^2
figure211_input1=[0.0 0.1 0.2 0.3];
figure211_input2=[0.5 0.55 0.6 0.65 0.7];
figure211_input3=[0.09 0.12 0.15];
figure211_Table(:,:,1)=[1.02  1.025 1.04  1.06  1.09
                        1.027 1.035 1.048 1.07  1.12
                        1.034 1.04  1.056 1.085 1.14
                        1.04  1.05  1.07  1.105 1.17
                       ];
figure211_Table(:,:,2)=[1.025 1.04  1.058 1.09  1.14
                        1.031 1.045 1.07  1.11  1.18
                        1.04  1.056 1.08  1.125 1.20
                        1.045 1.065 1.095 1.145 1.22
                       ];
figure211_Table(:,:,3)=[1.033 1.048 1.08  1.12  1.18
                        1.038 1.057 1.093 1.14  1.20
                        1.045 1.064 1.105 1.16  1.22
                        1.056 1.08  1.12  1.18  1.24
                       ];

% page195 Xd_A
figure231_input1=[0.06 0.1 0.15 0.2 0.25];
figure231_input2=[1.5 2.0 2.5 3.5 5 6 8 10];
figure231_Table=[0.46  .465 .457 .439 .414 .399 .37  .347
                  .433 .438 .427 .401 .368 .329 .32  .296
                  .392 .41  .395 .365 .338 .309 .284 .27
                  .34  .389 .37  .34  .305 .289 .27  .262
                  .28  .368 .353 .321 .29  .28  .265 .258
                ];

% page201 Xd_A a=5
figure237_5_input1=[0.0  0.2  0.333333  1.0];
figure237_5_input2=[-4.0  -3.5  -3.0  -2.5  -2.0  -1.5  -1.0  -0.5  0.0  0.5  1.0  1.5  2.0  2.5  3.0  3.5  4.0  4.5  5.0  6.0  8.0  12.0];
figure237_5_input3=[0.0  1.0  2.0  3.0];
figure237_5_Table(:,:,1)=[.263  .264  .264  .263  .263  .258  .250  .270  .326  .375  .410  .434  .449  .456  .462  .470  .473  .475  .477  .479  .479  .479 
                          .255  .256  .256  .251  .249  .241  .230  .240  .298  .351  .392  .427  .444  .454  .460  .464  .468  .472  .474  .476  .476  .476  
                          .245  .244  .240  .235  .230  .221  .200  .197  .258  .324  .375  .413  .435  .450  .456  .460  .465  .468  .470  .473  .473  .473  
                          .230  .230  .223  .220  .210  .193  .168  .140  .180  .260  .350  .387  .426  .442  .450  .455  .460  .463  .465  .468  .468  .468];  
figure237_5_Table(:,:,2)=[.277  .280  .290  .300  .310  .325  .350  .380  .408  .428  .441  .450  .453  .460  .462  .464  .466  .470  .471  .474  .474  .474  
                         .275  .275  .276  .278  .282  .300  .318  .347  .380  .410  .428  .440  .445  .450  .452  .454  .460  .462  .470  .472  .472  .472  
                         .255  .256  .257  .258  .257  .255  .253  .277  .321  .368  .398  .423  .438  .449  .451  .453  .457  .461  .463  .465  .465  .465  
                         .225  .224  .222  .220  .210  .195  .170  .170  .215  .295  .355  .389  .416  .430  .445  .450  .454  .458  .459  .460  .460  .460];  
figure237_5_Table(:,:,3)=[.330  .335  .342  .355  .370  .385  .415  .440  .465  .480  .489  .490  .489  .488  .488  .488  .488  .488  .488  .488  .488  .488  
                          .310  .315  .320  .326  .345  .350  .375  .405  .435  .465  .477  .480  .480  .481  .481  .481  .481  .481  .481  .481  .481  .481  
                          .277  .278  .279  .280  .285  .295  .312  .347  .386  .428  .452  .470  .476  .478  .480  .480  .480  .480  .480  .480  .480  .480  
                          .220  .220  .218  .217  .210  .200  .195  .210  .270  .330  .388  .421  .445  .462  .473  .475  .476  .477  .478  .478  .478  .478];  		
figure237_5_Table(:,:,4)=[.370  .375  .380  .395  .415  .430  .450  .475  .490  .507  .520  .525  .527  .527  .526  .525  .522  .520  .520  .521  .521  .521 
                          .340  .348  .355  .367  .377  .393  .420  .445  .472  .485  .507  .519  .520  .520  .519  .518  .516  .515  .514  .514  .514  .514   
                          .290  .293  .298  .305  .315  .325  .345  .375  .420  .445  .472  .484  .495  .502  .506  .507  .506  .504  .504  .504  .504  .504  
                          .205  .205  .205  .200  .198  .197  .202  .225  .292  .395  .417  .448  .474  .480  .495  .500  .500  .499  .498  .499  .499  .499];

% page201 Xd_A a=20
figure237_20_input1=[0.0 0.2 0.3333 1.0];
figure237_20_input2=[-2 -1 -0.5 0.0 0.5 1 2];
figure237_20_input3=[0.0 1 2 3];
figure237_20_Table(:,:,1)=[0.04  .07  .07  .065 .046 .03  .01
                            .072 .1   .1   .085 .065 .043 .012
                            .087 .125 .125 .105 .075 .05  .015
                            .1   .135 .135 .115 .085 .06  .02
                          ];
figure237_20_Table(:,:,2)=[0.0   .0   .0   .0   .0   .0   .0
                            .02  .04  .04  .038 .03  .02  .008
                            .045 .065 .065 .06  .045 .03  .01
                            .07  .09  .09  .08  .07  .05  .015
                          ];
figure237_20_Table(:,:,3)=[0.0   .0   .0   .0   .0   .0   .0
                            .0   .0   .0   .0   .0   .0   .0
                            .0   .03  .035 .035 .025 .02  .0
                            .03  .06  .06  .055 .05  .03  .0
                          ];
figure237_20_Table(:,:,4)=zeros(4,7);

% page205 Xdn 锥形头部与圆柱弹身压力中心系数
figure2311_input1=[0.0 0.1 0.3 0.5 0.75 1.0 1.5 2 3 4];
figure2311_input2=[-0.4 -0.3 -0.2 -0.1 0.0 0.1 0.2 0.3 0.5 1.0 1.5];
figure2311_Table=[0.58 .61 .64 .67 .67 .675 .68 .68 .68 .68  .68
                   .58 .61 .64 .67 .68 .685 .72 .72 .72 .72  .71
                   .58 .61 .64 .67 .69 .700 .76 .78 .78 .77  .76
                   .58 .61 .64 .67 .69 .710 .78 .81 .84 .84  .82
                   .58 .61 .64 .67 .70 .720 .80 .84 .88 .90  .88
                   .58 .61 .64 .67 .70 .730 .81 .86 .92 .95  .94
                   .58 .61 .64 .67 .70 .735 .81 .88 .96 1.04 1.05
                   .58 .61 .64 .67 .71 .740 .81 .88 .98 1.10 1.14
                   .58 .61 .64 .67 .71 .745 .81 .88 .99 1.17 1.26
                   .58 .61 .64 .67 .71 .750 .81 .88 .99 1.20 1.31  
                 ];

% page221 Xdt 锥形收缩尾部压力中心系数  
figure2327_input1=[0.0 0.1 0.2 0.3 0.35 0.45 0.5 0.8];
figure2327_input2=[0.1 0.2 0.4 0.5 0.6 0.8 1.0 1.5 2.0];
figure2327_Table=[0.397 .420 .452 .463 .470 .478 .482 .486 .486
                   .473 .500 .535 .548 .556 .568 .572 .578 .580
                   .500 .524 .555 .567 .574 .585 .591 .599 .602
                   .510 .535 .568 .580 .588 .597 .604 .610 .611
                   .520 .540 .572 .583 .592 .603 .610 .616 .618
                   .529 .548 .580 .590 .598 .610 .616 .623 .623
                   .537 .556 .585 .595 .604 .613 .620 .628 .630
                   .570 .582 .600 .609 .614 .620 .627 .632 .634    
                 ];

% page225 锥形头部-圆柱体因子G1
figure2331_input1=[2 4 5 8];
figure2331_input2=[5 10 14];
figure2331_Table=[2.25 5.20 7.70
                  1.80 5.00 7.50
                  1.30 4.56 7.25
                  0.75 4.10 6.90
                 ];

% page227 横流干扰因子G2
figure2333_input1=[0 5 10 15 20 25];
figure2333_input2=[1.0 1.5 2.5 3.5 4.0 5.0 6.0 7.0 7.5];
figure2333_Table=[0.20 0.23 0.34 0.55 0.70 0.90 0.88 0.87 0.87
                  0.44 0.54 0.67 0.95 1.04 1.10 1.03 1.00 1.00
                  0.74 0.78 1.05 1.26 1.27 1.18 1.06 1.00 1.00
                  1.31 1.34 1.44 1.44 1.37 1.22 1.10 1.00 1.00
                  1.93 1.87 1.73 1.52 1.43 1.25 1.11 1.00 1.00
                  1.95 1.89 1.73 1.52 1.43 1.25 1.11 1.00 1.00
                 ];

% page228 f1
figure2334_input=[0.03  0.05  0.10  0.15  0.20  0.30  0.40  0.50  0.60  0.70  0.80  0.90  1.00];
figure2334_Table=[.0275  .0338  .0385  .0400  .0401  .0368  .0293  .0200  .0118  .0062  .0025  .0008  .0000];

% page229 f2
figure2335_input=[0.0  0.1  0.2  0.3  0.4  0.5  0.6];
figure2335_Table=[1.04  1.00  0.96  0.92  0.88  0.84  0.80];

% page230 翼对体的干扰参数 f(D/Lw')
figure2336_input=[0.0 0.05 0.1 0.2 0.3 0.4 0.5];
figure2336_Table=[0.0 0.098 0.152 0.218 0.263 0.3 0.33];
%--------------------------------------------------------------------------

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