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前机身对飞机大迎角气动特性的影响 被引量:1

Influence of Forebody on Aerodynamic Characteristics of Aircraft High Angles of Attack
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摘要 通过对一些相关文献的分析,得出了前机身外形是要求具有过失速机动能力的飞机气动设计的关键这一结论,并建议在气动布局工作中加强对前机身特性研究。 By analyzing series of relative research of aircrafts with good high AOA characteristic, conclusion is made that the forebody design is the key factor of aircraft aerodynamic design that require post-stall maneuver. Recommendation is also made on the future research of forebody design on aircraft configuration research.
出处 《飞机设计》 2011年第6期6-9,15,共5页 Aircraft Design
关键词 前机身 大迎角 过失速 forebody high angles of attack poststall
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参考文献5

  • 1Hunt B L. Asymmetric vortex force and wakes on slender bodies[R]. AIAA-82-1336, 1982.
  • 2Edwards O R. Northrop F-5F shark nose development[R]. NASACR-158936, 1978.
  • 3Chambers J R. High-angle-of-attack aerodynamics: lessons learned[R]. AIAA-86-1774, 1986.
  • 4Alcorn C W, Croom M A, Francis M S. The X-31 experience: aerodynamic impediments to post-stall agility[R]. AIAA-95- 0362, 1995.
  • 5Clark C, Bernens M. High angle-of-attack flight characteristics of the YF-22[R]. AIAA-91-3194, 1991.

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