| 论机动飞机机体/进气道一体化 |
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| 引用本文： | 杨国才.论机动飞机机体/进气道一体化[J].推进技术,1999,20(2):103-107. |
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| 作者姓名： | 杨国才 |
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| 作者单位： | 成都飞机设计研究所,成都,610041 |
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| 摘 要： | 机动飞机／发动机一体化，一直是多年来国际上研制高机动性战斗机中不容忽视的一项重大课题，目的在于提高发动机包括进气道、尾喷管在内的推进系统的工作效率和稳定性。列举了国外的一些型号，特别是有分叉进气道战斗机在研制中必须加以考虑的一体化问题，并从设计原理的角度，给出了一些旨在提高性能与安全性的可供选择的进气道构形。
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| 关 键 词： | 高机动性飞机，飞机－发动机匹配，进气道－发动机匹配，一体化设计 |
| 修稿时间： | 1998-04-24 |
REVIEW OF AIRFRAME/INLET INTEGRATION OF MANEUVER FIGHTER AIRCRAFT |
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| Yang Guocai.REVIEW OF AIRFRAME/INLET INTEGRATION OF MANEUVER FIGHTER AIRCRAFT[J].Journal of Propulsion Technology,1999,20(2):103-107. |
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| Authors: | Yang Guocai |
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| Institution: | Chengdu Aircraft Design and Research Inst.,Chengdu,610041 |
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| Abstract: | Aircraft
airframe/engine integration has been always a major attention getting subject in maneuver
fighter aircraft development internationally for the years,aiming at inproving the operating
effectiveness and stability of propulsion system including inlet and nozzle.This paper lists the
integration examples of some foreign fighter types,especially those of symmetrical twin intake
air induction systems,and gived the alternative inlet configuration with the intention of
performance and safety inprovements as viewed from fundamentals of fighter design. |
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| Keywords: | ighly maneuverable aircraft Airplane engine matching Inlet engine matching Integrated design |
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