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Description: THEY MUST BE CHANGES TO COMMENT CARDS BEFORE COMPILING IN
C*** FORTRAN-IV.
CTHEY MUST BE CHANGES TO COMMENT CARDS BEFORE COMPILING IN
C*** FORTRAN-IV.
C
Platform: |
Size: 43008 |
Author: l454216@mvrht.net
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Description: C*** NOTE - WHEN CONVERTING FROM FORTRAN-IV TO FORTRAN-V THE
Platform: |
Size: 12288 |
Author: l454216@mvrht.net
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Description: THIS PROGRAM REQUIRES SEVERAL TAPE UNITS FOR I/O. THESE ARE
C*** DEFINED IN FORTRAN-VTHESE ARE
C*** DEFINED IN FORTRAN-V
Platform: |
Size: 13312 |
Author: l454216@mvrht.net
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Description: C PROGRAM DATCOM(INPUT=100,OUTPUT,TAPE5=INPUT,TAPE6=OUTPUT,
C 1 TAPE8=100,TAPE9=100,TAPE10=100,TAPE11=100,
C 2 TAPE12,TAPE13,TAPE14)
Platform: |
Size: 444416 |
Author: l454216@mvrht.net
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Description: 可用于计算机翼或全机低速飞行时的气动力，计算结果可以直接被matlab调用(Calculate the aerodynamic forces of a wing or whole aircraft at low speeds)
Platform: |
Size: 30106624 |
Author: abao520
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Description: 导弹气动参数计算，气动外形设计，适用于大多数大气层内飞行的导弹。非常好用，赶快下载。(Achieve missile aerodynamic parameter calculation, calculation of various aerodynamic parameters)
Platform: |
Size: 1284096 |
Author: a9b8
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Description: missile DATCOM-corrected version
Platform: |
Size: 910336 |
Author: hmsa |
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Description: MD_GUI_Ver_3.6.0_Portable
Platform: |
Size: 1111040 |
Author: NguyenDinhDuong |
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Description: Missile Datcom's GUI Manual
Platform: |
Size: 10532315 |
Author: kiwijuice |
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Description: GUI version of missiledatcom. The aerodynamic parameters, including drag coefficient, lift coefficient and torque coefficient, can be calculated quickly by inputting missile shape parameters.
Platform: |
Size: 45143987 |
Author: 2239538092@qq.com |
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Description: In preliminary design operations, rapid and economical estimations of
aerodynamic stability and control characteristics are frequently required. The
extensive application of complex automated estimation procedures is often
prohibitive in terms of time and computer cost in such an environment.
Platform: |
Size: 4214285 |
Author: chenqua |
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