Computational Study of the Asymptotic Flow Structure of a High-Aspect-Ratio Swept Wing in Transonic Flow-Reference-Cited by-同舟云学术

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Computational Study of the Asymptotic Flow Structure of a High-Aspect-Ratio Swept Wing in Transonic Flow

Published:1982 Issue: Volume: Page:107-145
ISSN:
Container-title:Transonic, Shock, and Multidimensional Flows
language:
Short-container-title:

Author:

Cheng H.K.

Publisher

Elsevier

Reference65 articles.

1. Busemann, A., Aerodynamischer Auftrieb bei Überschallgeschwindigkeit, Luftfahrtforschung Bd 12, Nr. 6, 1975, 210-220.

2. Jones, R.T., Wing Planform for High Speed Flight, NACA Report 863, 1945.

3. Aerodynamics of Wings at High Speed;Jones,1957

4. Aerodynamic Design;Küchemann;The Aeronautical Journal,1969

5. Reduction of Wave Drag by Antisymmetric Arrangement of Wings and Bodies;Jones;AIAA J.,1972

Cited by 1 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. Lunate-tail swimming propulsion as a problem of curved lifting line in unsteady flow. Part 1. Asymptotic theory;Journal of Fluid Mechanics;1984-06

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