Computational and simplified analytical treatment of transonic wing-fuselage-pylon-store interactions-Reference-Cited by-同舟云学术

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Computational and simplified analytical treatment of transonic wing-fuselage-pylon-store interactions

Published:1980-01-14 Issue: Volume: Page:
ISSN:
Container-title:18th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

SHANKAR V.¹,MALMUTH N.¹

Affiliation:

1. Rockwell International Science Center, Thousand Oaks, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1980-127

Reference9 articles.

1. Shankar,V., Malmuth, N.D., and Cole, J.D. "A Comoutational Transonic Inverse Procedure for Thkee-Dimensional Wings and Wing-Body Combinations," AIM Paper No. 79-0344. Also to appear in AIM Journal.

2. Alford, W.J. and King,T.J. "Experimental Static and Aerodynamic Forces and Moments at High Subsonic Speeds on a Missile Model during Simulated Launching from a Semispan Location of a 45' Swept-Wing-Fuselage-PylonCombination." NACA Report RML56J05, January 10,1957.

Cited by 3 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. A new approach to weapon separation aerodynamics;Journal of Aircraft;1982-12

2. A new approach to weapon separation aerodynamics;Aircraft Systems and Technology Conference;1981-08-11

3. A grid interfacing zonal algorithm for three-dimensional transonic flows about aircraft configurations;Eighth International Conference on Numerical Methods in Fluid Dynamics

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