Simulated transonic flows for aircraft with nacelles, pylons, and winglets
Author:
Affiliation:
1. Grumman Aerospace Corp., Bethpage, N.Y.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1980-130
Reference19 articles.
Cited by 35 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. Transonic flow computations using nonlinear potential methods;Progress in Aerospace Sciences;2000-01
2. UNSTEADY TRANSONIC POTENTIAL FLOW OVER A FLEXIBLE FUSELAGE;34th Structures, Structural Dynamics and Materials Conference;1993-04-19
3. Estimation of propulsion-induced effects on transonic flows over a hypersonic configuration;30th Aerospace Sciences Meeting and Exhibit;1992-01-06
4. Unsteady transonic flow calculations for realistic aircraft configurations;Journal of Aircraft;1989-01
5. Winglets on low-aspect-ratio wings;Journal of Aircraft;1988-10
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