期刊文献+

“升力推力”飞行器技术分析

Analysis of Technique for "Lift Thrust" Aircraft
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摘要 大气层中的高超声速巡航飞行,将是继喷气发动机时代之后航空发展的又一里程碑,而飞行器设计的"升阻比"屏障也是继热障、黑障之后的又一技术关键。"升力推力"飞行器是根据新世纪对高超声速飞行器的需求提出的一种新型飞行器概念,它可以使飞行器的升阻比得以有效提高。本文对"升力推力"飞行器概念及其动力进行了技术分析,并对其未来的发展进行了展望。 Followed the age of jet engine, the hypersonic cruise flight in the aerosphere will be another milestone in the development of aviation. Lift-drag ratio barrier in aircraft design will become another technique crux after thermal barrier and black barrier. "Lift thrust" aircraft is a new type of aircraft presented for the requirement of hypersonic aircraft in the new century. It can allow the lift-drag ratio of the aircraft enhanced effectively. This paper made some analysis on techniques of the concept and power for the "lift-thrust" aircraft, and looked into its future development.
出处 《燃气涡轮试验与研究》 2009年第3期57-59,共3页 Gas Turbine Experiment and Research
关键词 升力推力 高超声速 飞行器 动力 lift-thrust hypersonic aircraft power
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参考文献3

  • 1Groeco L.High Speed Aerodynamics and Jet Propulsion:Vol.Ⅲ[M].Princeton:Princeton University Press,1959.
  • 2Baldwin B S.Application to Fluid Dynamics of the Theory of Reversible Heat Addition[R].NASA TN-D-93,1959.
  • 3Prandtl L.流体力学概论[M].郭永怀,陆士嘉,译.北京:科学出版社,1981.

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