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推重比—10级发动机综述

The summarization of grade 10 thrust/weight ratio engines
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摘要 本文首先介绍了第四代战斗机及其动力装置的战术技术要求 ,分析了国外推重比 10一级发动机的设计技术 ,并通过对飞机推重比和发动机推重比的关系、飞机推力与飞行器阻力之间的夫系 ,对我国推重比 10—级发动机提出了技术要求。 This paper first on troduces a tactical and technological requirement to the fourth generation of fighter planes and their power plant.The paper then analizes the design technique of foreign grade 10 thrust/weight ratio engines.Finally,some technical requirement and parameter choice are proposed for the native grade 10 thrust/weight ratio engines,based on the relationship between thrust/weight ratio of the aircraft and engine and the relationship between the aircraft thrust and resistance.
出处 《沈阳航空工业学院学报》 2003年第1期17-19,共3页 Journal of Shenyang Institute of Aeronautical Engineering
关键词 战斗机 动力装置 推重比 核心机 发动机 设计 参数选择 Air fighter engine thrust/weight ratio core engine
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参考文献2

  • 1Rapp, G. C. The F404 Development Program - A New Approach.ALAA Paper AIA -82 - 1180, AIAA/SAE/ASME 18t h Joint Propulsion Conference, Cleveland Ohio. AIKA, New York, N. Y.June, 1982.
  • 2Daub, W. J, Larsson, L, Veno, L B. Development of the F404/RM 12 for the JAS39 Gripen ,. ASME Paper 88 - GT - 305, ASME Gas Turbine and Aeroengine Conqress. Amsterda, The Netherlauds. ASME, New York, N. Y. june, 1988.

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