Redesign of a supercritical wing in the presence of an engine nacelle-Reference-Cited by-同舟云学术

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Redesign of a supercritical wing in the presence of an engine nacelle

Published:1987-12 Issue:2 Volume:73 Page:233-243
ISSN:0021-9991
Container-title:Journal of Computational Physics
language:en
Short-container-title:Journal of Computational Physics

Author:

Ross David S

Publisher

Elsevier BV

Subject

Computer Science Applications,Physics and Astronomy (miscellaneous),Applied Mathematics,Computational Mathematics,Modeling and Simulation,Numerical Analysis

Reference10 articles.

1. A Theory of Supercritical Wing Sections With Computer Programs and Examples;Bauer,1972

2. Supercritical Wing Sections II, a Handbook;Bauer,1975

3. Supercritical Wing Sections III;Bauer,1977

4. The NYU Inverse Swept Wing Code;Bauer;NASA CR3662,1983

5. Technique for developing design tools from the analysis methods of computational aerodynamics;Davis;AIAA Paper 79-1529,1979

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. Inviscid drag prediction for transonic transport wings using a full-potential method;Journal of Aircraft;1991-12

2. Innovative pylon concepts for engine-airframe integration for transonic transports;20th Fluid Dynamics, Plasma Dynamics and Lasers Conference;1989-06-12

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