A Foward-Swept-Wing Fighter Configuration Designed by a Transonic Computational Method-Reference-Cited by-同舟云学术

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A Foward-Swept-Wing Fighter Configuration Designed by a Transonic Computational Method

Published:1986-06 Issue:6 Volume:23 Page:506-512
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Mann Michael J.¹,Mercer Charles E.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.56774

Reference26 articles.

1. Wind tunnel investigation of the transonic aerodynamic characteristics of forward swept wings

2. 5Spacht, G. "The Forward Swept Wing: A Unique Design Challenge," AIAA Paper 80-1885, Aug.1980.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Pressure measurements on a forward-swept wing-canard configuration;Journal of Aircraft;1994-03

2. Experimental study on the aerodynamic effects of a forward-sweep angle;Journal of Aircraft;1993-09

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