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火箭飞行性能 (SOAR程序,可与固体火箭发动机设计软件共用)

2018-3-31 19:24| 发布者: dymodel| 查看: 155| 评论: 0|原作者: 百度

摘要: 这一计划预计飞行性能的火箭。 It calculates parameters such as altitude, velocity, acceleration, drag force, dynamic pressure, Mach number, and is capable of handling single-stage, multi-stage and clus ...
这一计划预计飞行性能的火箭。 It calculates parameters such as altitude, velocity, acceleration, drag force, dynamic pressure, Mach number, and is capable of handling single-stage, multi-stage and clustered rockets.计算参数,如高度,速度,加速度,曳力,动态压力,马赫数,并能够处理单阶段,多阶段和群集火箭。 Meant to be accurate, the program utilizes efficient professional subroutines for numerical differentiation and integration.意思是准确的,该计划利用高效率的专业子程序数值分化和整合。 Also meant to be versatile and user friendly, it can handle supersonic rockets with a flight ceiling to 100,000 feet.还意味着要灵活和用户友好的,它可以处理火箭与超音速飞行上限十点零零万英尺。 as easily as low altitude model rockets with commercial engines.一样简单低空模型火箭,与商业引擎。 Runs under DOS only.运行在DOS下而已。 Written by Richard Nakka & BW Nakka.书面理查德nakka &体重nakka 。

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