122mm火箭弹弹道计算程序c++.

上传者: mingge1027 | 上传时间: 2019-12-21 20:19:33 | 文件大小: 2.16MB | 文件类型: rar
122mm火箭弹弹道计算程序c++.大家看看吧

文件下载

资源详情

[{"title":"( 37 个子文件 2.16MB ) 122mm火箭弹弹道计算程序c++.","children":[{"title":"122mm火箭弹弹道计算程序c++","children":[{"title":"MissileTrajectorySimulation.opt <span style='color:#111;'> 47.50KB </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulation_Output.dat <span style='color:#111;'> 113.68KB </span>","children":null,"spread":false},{"title":"chongliang.h <span style='color:#111;'> 85B </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulation.h <span style='color:#111;'> 1.22KB </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulation.ncb <span style='color:#111;'> 65.00KB </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulation.plg <span style='color:#111;'> 1.33KB </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulation.dsp <span style='color:#111;'> 3.57KB </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulationRk.Cpp <span style='color:#111;'> 356B </span>","children":null,"spread":false},{"title":"lbg.h <span style='color:#111;'> 1.28KB </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulationRk.h <span style='color:#111;'> 405B </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulation.dsw <span style='color:#111;'> 562B </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulation.Cpp <span style='color:#111;'> 4.71KB </span>","children":null,"spread":false},{"title":"53度射角数据","children":[{"title":"带阻力环高温弹道诸元数据.dat <span style='color:#111;'> 433.91KB </span>","children":null,"spread":false},{"title":"低温弹道诸元数据.dat <span style='color:#111;'> 453.34KB </span>","children":null,"spread":false},{"title":"带阻力环常温弹道诸元数据.dat <span style='color:#111;'> 431.76KB </span>","children":null,"spread":false},{"title":"带阻力环低温弹道诸元数据.dat <span style='color:#111;'> 424.55KB </span>","children":null,"spread":false},{"title":"高温弹道诸元数据.dat <span style='color:#111;'> 463.75KB </span>","children":null,"spread":false},{"title":"常温弹道诸元数据.dat <span style='color:#111;'> 461.25KB </span>","children":null,"spread":false}],"spread":true},{"title":"MissileTrajectorySimulation_Input.dat <span style='color:#111;'> 780B </span>","children":null,"spread":false},{"title":"通用弹道仿真计算程序(经典版).txt <span style='color:#111;'> 510B </span>","children":null,"spread":false},{"title":"Debug","children":[{"title":"MissileTrajectorySimulation_Output.dat <span style='color:#111;'> 0B </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulation.pch <span style='color:#111;'> 236.85KB </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulation.ilk <span style='color:#111;'> 252.87KB </span>","children":null,"spread":false},{"title":"vc60.idb <span style='color:#111;'> 73.00KB </span>","children":null,"spread":false},{"title":"vc60.pdb <span style='color:#111;'> 52.00KB </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulation.obj <span style='color:#111;'> 19.61KB </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulation.pdb <span style='color:#111;'> 537.00KB </span>","children":null,"spread":false},{"title":"MissileTrajectorySimulation.exe <span style='color:#111;'> 232.14KB </span>","children":null,"spread":false}],"spread":false},{"title":"MissileTrajectorySimulation.exe <span style='color:#111;'> 228.11KB </span>","children":null,"spread":false},{"title":"10度射角数据","children":[{"title":"带阻力环高温弹道诸元数据.dat <span style='color:#111;'> 110.74KB </span>","children":null,"spread":false},{"title":"低温弹道诸元数据.dat <span style='color:#111;'> 107.31KB </span>","children":null,"spread":false},{"title":"带阻力环常温弹道诸元数据.dat <span style='color:#111;'> 108.94KB </span>","children":null,"spread":false},{"title":"带阻力环低温弹道诸元数据.dat <span style='color:#111;'> 104.81KB </span>","children":null,"spread":false},{"title":"高温弹道诸元数据.dat <span style='color:#111;'> 113.68KB </span>","children":null,"spread":false},{"title":"常温弹道诸元数据.dat <span style='color:#111;'> 111.71KB </span>","children":null,"spread":false}],"spread":false}],"spread":false},{"title":"弹道估算.pdf <span style='color:#111;'> 249.57KB </span>","children":null,"spread":false},{"title":"内弹道仿真程序Chamber Interior Ballistics--C源代码.rar <span style='color:#111;'> 828.90KB </span>","children":null,"spread":false}],"spread":true}]

评论信息

  • oPangLong :
    好好学习一下
    2018-09-04
  • tolence :
    程序内容翔实,看着好像是导弹飞行力学后面所附程序
    2016-08-30
  • 狒狒空空 :
    对初学者比较有帮助,谢谢分享!
    2016-08-05
  • baidu_26587149 :
    谢谢分享,是质点弹道方程
    2015-10-15
  • popuwal :
    对我没有很大用途,但相信会对别人有用
    2014-06-29

免责申明

【只为小站】的资源来自网友分享,仅供学习研究,请务必在下载后24小时内给予删除,不得用于其他任何用途,否则后果自负。基于互联网的特殊性,【只为小站】 无法对用户传输的作品、信息、内容的权属或合法性、合规性、真实性、科学性、完整权、有效性等进行实质审查;无论 【只为小站】 经营者是否已进行审查,用户均应自行承担因其传输的作品、信息、内容而可能或已经产生的侵权或权属纠纷等法律责任。
本站所有资源不代表本站的观点或立场,基于网友分享,根据中国法律《信息网络传播权保护条例》第二十二条之规定,若资源存在侵权或相关问题请联系本站客服人员,zhiweidada#qq.com,请把#换成@,本站将给予最大的支持与配合,做到及时反馈和处理。关于更多版权及免责申明参见 版权及免责申明