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Description: 用神经网络实现六自由度平台的姿态症结问题-using neural network platform 6-DOF posture crux of the problem
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Size: 1024 |
Author: 刘砜 |
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Description: 介绍了子母弹气动干扰风洞实验新方案的特点及实验装置的构成。利用该方案进行了布撒
器 —子弹气动干扰风洞实验。-Describes the shrapnel Aerodynamic wind tunnel tests of the new program features and the composition of experimental devices. Using the program was Dispenser- Bullet aerodynamic interference wind tunnel experiment.
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Size: 174080 |
Author: 王顺红 |
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Description: 美国空军标准的飞行器气动计算软件DATCOM的可视化版本，使用更加方便！-A software with GUI, which can be used to calculate aerodynamic characteristics of a aircraft!
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Size: 827392 |
Author: 策划家 |
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Description: NSEG是美国兰利研究中心推出的飞行器起飞、爬升、巡航、加速、下降、减速和着陆等各个过程分析软件。-NSEG was developed to perform rapid aircraft mission analyses. It is based upon the
use of approximate equations of motion whose form varies with the type of flight
segment. Flight segments considered are takeoff, accelerations, climbs, cruises, descents,
decelerations, and landings. Layered atmosphere options are available. The program can
also be used for flight envelope mapping. NSEG provides the capability to analyze
aircraft missions from low to hypersonic speeds. Realistic and detailed vehicle
characteristics are input to NSEG to permit accurate mission analysis. NSEG allows
engine scaling so as to fit the design under analysis. NSEG contains several approximate
flight path optimization capabilities based on Rutowski energy-like criteria for
considering minimum time or fuel flight segments and maximum range segments during
climb or descent. Takeoff and landing analysis is based on the Air Force Flight
Dynamics Laboratory DATCOM method of high lift aerodynamic modelling
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Size: 150528 |
Author: 李喜 |
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Description: 实现导弹的气动参数计算，各种气动参数的计算。-Achieve missile aerodynamic parameter calculation, calculation of various aerodynamic parameters.
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Size: 7475200 |
Author: 韩治国 |
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Description: missile data compendium
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Size: 1285120 |
Author: SYG |
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Description: the pdf file of AIAA journal paper which was downloaded from its site and it is about MD(missile datcom)
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Size: 296960 |
Author: mohammad |
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Description: 弹道计算工具，包括文档说明，和相关源代码，好东西-Ballistic calculation tools, including documentation, and related source code, good things
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Size: 1986560 |
Author: 王王 |
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Description: 气动计算软件DATCOM，美国空军用，飞行器设计初期气动参数估算很好的软件。-Aerodynamic calculation software DATCOM, the United States Air force used, the initial design of aircraft aerodynamic parameter estimation is very good software.
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Size: 1410048 |
Author: 陈现象 |
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Description: Missile datcom revision 2011 GUI
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Size: 45475840 |
Author: anton |
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Description: 通用导弹气动力计算程序,由美国空军开发，比较实用且简单易学-Common Missile aerodynamic calculation program, developed by the Air Force, more practical and easy to learn
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Size: 613376 |
Author: 逍遥游 |
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Description: 飞机类快速计算软件，很好用，快速工程算法(Aircraft rapid calculation software)
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Size: 1410048 |
Author: yueliangm
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Description: C*** END-OF-FILE CHECKS IN ROUTINES CONERR, INPUT, READCD, AND XPERNM
C*** MUST BE CHANGED. THE CORRECT CODE IS GIVEN IN THE
C*** APPROPIATE PLACES OF EACH ROUTINE. REPLACE THE C IN COLUMN 1
C*** WITH A BLANK AND ON THE CARDS IDENTIFIED AS FORTRAN-V
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Size: 32768 |
Author: l454216@mvrht.net
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Description: REPLACE THE C IN COLUMN 1
C*** WITH A BLANK AND ON THE CARDS IDENTIFIED AS FORTRAN-V
C*** REPLACE THE BLANK IS COLUMN 1 WITH A C.
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Size: 24576 |
Author: l454216@mvrht.net
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Description: C*** NOTE - WHEN CONVERTING FROM FORTRAN-IV TO FORTRAN-V THE
C*** END-OF-FILE CHECKS
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Size: 18432 |
Author: l454216@mvrht.net
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Description: Datcom compiler exibition
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Size: 64512 |
Author: CesareBB |
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Description: 基于f语言的datcom气动参数计算软件，有界面，版本较老 但是可运行(Datcom pneumatic parameter calculation software based on f language, the version is older but can run)
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Size: 2829312 |
Author: wanglu888 |
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Description: MISSILE DATCOM User Manual, 2011 Revision
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Size: 2191360 |
Author: lolwut720 |
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Description: This is digital datcom source code.
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Size: 644453 |
Author: peyertrump |
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