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舰载蒸汽弹射内弹道设计计算
引用本文:陈庆贵,齐强,林琨山,周红梅.舰载蒸汽弹射内弹道设计计算[J].舰船科学技术,2012,34(6):107-110.
作者姓名:陈庆贵  齐强  林琨山  周红梅
作者单位:1. 海军航空工程学院,山东烟台,264001
2. 中国人民解放军91604部队,山东龙口,265700
摘    要:应用导弹发射内弹道原理,建立了舰载蒸汽弹射内弹道设计与计算模型。并以某型飞机为例,对所建立的内弹道设计与计算模型进行了仿真计算。仿真结果表明,所建立的模型能较好地满足内弹道设计指标要求,这对舰载蒸汽弹射装置的设计与工程研制具有一定的参考价值。

关 键 词:蒸汽弹射  内弹道  舰载机

Interior ballistic design and computation for the steam ejecting of carrier plane
CHEN Qing-gui , QI Qiang , LIN Kun-shan , ZHOU Hong-mei.Interior ballistic design and computation for the steam ejecting of carrier plane[J].Ship Science and Technology,2012,34(6):107-110.
Authors:CHEN Qing-gui  QI Qiang  LIN Kun-shan  ZHOU Hong-mei
Institution:1(1.Naval Aeronautical and Astronautical University,Yantai 264001,China; 2.No.91604 Unit of PLA,Longkou 265700,China)
Abstract:Interior ballistic design and computation models for the steam ejecting of carrier plane were established by applying theories of missile launching interior ballistic.One type of plane was taken for example to compute equations of interior ballistic design and computation.Results showed that established models could meet the demands on interior ballistic parameters.This is of some reference value for the design and engineering manufacture of steam-powered ejecting vehicle.
Keywords:steam ejecting  interior ballistic  carrier plane
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