搜索资源列表
RocketModeler
- 火箭造型设计和飞行模拟器 -Rocket Modeler can be used as a simulator that models the design and flight of a can modelrocket
height
- 这段源程序是用来计算火箭发动机的高度特性。-to calculate the height of the rocket engine.
simulating-combustion-flow-in-rocket-chamber
- simulation combustion
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- 固体_液体火箭发动机环境下3DC_SiC喉衬烧蚀性能实验.-Solid _ liquid rocket engine environment 3DC_SiC Throat ablation performance test.
huojiandandaojisuan
- 计算火箭飞行的弹道。采用欧拉法，龙哥库塔近似计算火箭飞行弹道。-Calculation of the rocket flight trajectory. Using Euler method, Long Ge Kuta approximate rocket flight trajectory.
pressure-established
- 端面燃烧固体火箭发动机压强建立过程计算程序 输入为比热比，燃气气体常数，点火温度，推进剂密度，装药直径，喷管喉部直径，装药体积，燃速相关常数 输出为压强和工作时间-Face charge calculation of solid rocket motor process of establishing the working pressure Input for the specific heat ratio, gas gas c
tube-charge-pressure-established
- 管型燃烧固体火箭发动机压强建立过程计算程序 输入为比热比，燃气气体常数，点火温度，推进剂密度，装药直径（内径和外径），喷管喉部直径，装药体积，燃速相关常数 输出为压强和工作时间-tube type of solid rocket motor combustion pressure build process calculation programs for heat input than, gas gas constant, the i
star-charge-pressure-established
- 管型燃烧固体火箭发动机压强建立过程计算程序 输入为比热比，燃气气体常数，点火温度，推进剂密度，星角数，星角度大小，装药直径（内径和外径），喷管喉部直径，装药体积，燃速相关常数 输出为压强和工作时间-Star of solid rocket motor combustion pressure build process calculation programs for heat input than, gas gas constant,
Rocket_Design
- Rocket systems are presented in two broad classes: military rocket systems and research rocket systems. Military rocket systems are discussed in terms of their application in a battle environment. Research rocket systems
ProjectCode
- The objective is to find out the time at which the rocket reaches a speed of 1000m/s (3600km/hr). Analysis We know the following: * Initial mass of the rocket and fuel, 160000kg, or 160 metric tons. * Fuel combus
eightCoins
- 八硬币经典解决方案,较多注释.通过三次称量找出不同的那枚硬币-Eight coins classical solutions, more annotations to identify the different coins of the rocket through three weighing
VC6_Cpp_MFC
- vc模拟卫星发射全过程-vc stimulate rocket
075
- 火箭发射图形源码,是用纯C语言描述的模拟火箭发射的图形-rocket map
MOC_NOzzle3D
- computer program for the calculation of steady three dimensional adiabatic flows in supersonic rocket engine nozzles. The fluid is assumed to be an inviscid perfect gas and the flow is assumed to be shock free. The gover
SRM_IGN
- Prediction and control of the pressure-time and thrust time programs of high-performance solid propellant rocket motors
rocketperf
- A matlab scr ipt to calculate the performance of a multi-stage rocket. payloads, veloicties, all dem good stuffs.-A matlab scr ipt to calculate the performance of a multi-stage rocket. payloads, veloicties, all dem good
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- 火箭发射演示 火箭发 射演示 -Rocket launchers demoRocket launchers demoRocket launchers demoRocket launchers demo
missile
- 用于计算固体火箭弹道的仿真实例程序，绘制弹道仿真图像-Simulation example is used to calculate the trajectory of the solid rocket program, draw a trajectory simulation image
zuozuishadeyuangong
- 提起杨丽，大家无不惊叹于她创造的升迁神话。高职毕业之后，在本科生云集研究生成群的大公司从前台接待做起，然后就以火箭般的速度，在三年内登上了部门经理的宝座。是突来的神力炼就了过人的聪慧，还是侥幸的好运，大家众说纷纭。但我知道，从前台到经理，她一直是公司里最傻的员工。-Filed Yang Li, we all marvel at the promotion myth she created. After graduation from h
Random_generate
- 进行数据分析，帮助初学者掌握常用matlab算例，功能在于火箭推法-Data analysis to help beginners to master commonly matlab example, function is the rocket extrapolation