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【Other】 src DL : 0: 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
Update : 2024-05-06 Size : 43008 Publisher : l454216@mvrht.net
【Other】 4444455e DL : 0: C*** NOTE - WHEN CONVERTING FROM FORTRAN-IV TO FORTRAN-V THE
Update : 2024-05-06 Size : 12288 Publisher : l454216@mvrht.net
【matlab】 3333e DL : 0: THIS PROGRAM REQUIRES SEVERAL TAPE UNITS FOR I/O. THESE ARE C*** DEFINED IN FORTRAN-VTHESE ARE C*** DEFINED IN FORTRAN-V
Update : 2024-05-06 Size : 13312 Publisher : l454216@mvrht.net
【Special Effects】 111e DL : 0: 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)
Update : 2024-05-06 Size : 444416 Publisher : l454216@mvrht.net
【transportation applications】 Datcom DL : 1: 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)
Update : 2024-05-06 Size : 30106624 Publisher : abao520
【Other】 MISSILE DATCOM DL : 3: 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)
Update : 2024-05-06 Size : 1284096 Publisher : a9b8
【Other】 missile_datcom_2011_download DL : 4: missile DATCOM-corrected version
Update : 2024-05-06 Size : 910336 Publisher : hmsa
【Other】 OpenPost-master DL : 1: MD_GUI_Ver_3.6.0_Portable
Update : 2024-05-06 Size : 1111040 Publisher : NguyenDinhDuong
【Other】 MissileLab User Guide DL : 1: Missile Datcom's GUI Manual
Update : 2022-04-12 Size : 10532315 Publisher : kiwijuice
【Compiled】 Missile Datcom 2011 GUI DL : 5: GUI version of missiledatcom. The aerodynamic parameters, including drag coefficient, lift coefficient and torque coefficient, can be calculated quickly by inputting missile shape parameters.
Update : 2022-10-19 Size : 45143987 Publisher : 2239538092@qq.com
【Software Engineering】 Digital Datcom+ new version DL : 1: 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.
Update : 2023-09-13 Size : 4214285 Publisher : chenqua

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