| 舰载机弹射内弹道仿真计算 |
| |
| 引用本文： | 齐强,孙建国,周源,周红梅.舰载机弹射内弹道仿真计算[J].海军航空工程学院学报,2009,24(5):507-510. |
| |
| 作者姓名： | 齐强 孙建国 周源 周红梅 |
| |
| 作者单位： | 1. 海军航空工程学院七系,山东,烟台,264001
2. 海军航空工程学院新装备培训中心,山东,烟台,264001 |
| |
| 摘 要： | 建立了舰载机弹射内弹道方程组和蒸汽流量方程，根据内弹道设计指标要求和飞机参数对弹射过程进行了仿真计算。仿真计算结果表明，内弹道参数及供汽规律能够满足设计指标要求，可以为舰载机弹射器的工程设计提供理论依据。
|
| 关 键 词： | 蒸汽弹射 内弹道方程组 仿真计算 |
Inner Launch-Trajectory Simulation for Deck-Landing Aircrafts |
| |
| QI Qiang,SUN Jian-guo,ZHOU Yuan and ZHOU Hong-mei.Inner Launch-Trajectory Simulation for Deck-Landing Aircrafts[J].Journal of Naval Aeronautical Engineering Institute,2009,24(5):507-510. |
| |
| Authors: | QI Qiang SUN Jian-guo ZHOU Yuan and ZHOU Hong-mei |
| |
| Institution: | ( Naval Aeronautical and Astronautical University 1.N27 Department; 2. New Equipment Training Center, Yantai Shandong 264001, China) |
| |
| Abstract: | The inner launch-trajectory equations and vapor-discharge equation for deck-landing aircrafts were established. According to the required design indexes of inner launch-ballistic and the take-off indexes of aircraft, the aircraft launch-off process was simulated. The simulation results demonstrated that, the inner launch-ballistic dynamic parameter and the vapor-discharge regularity are able to satisfy the design indexes. This method can provide theoretical basis for the engineering design of aircraft ejection power plant. |
| |
| Keywords: | vapor ejection power plant inner launch-trajectory equations simulation |
| 本文献已被 维普 万方数据 等数据库收录！ |
| 点击此处可从《海军航空工程学院学报》浏览原始摘要信息 |
| 点击此处可从《海军航空工程学院学报》下载免费的PDF全文 |
