A TRANSONIC MUTUAL INTERFERENCE PROGRAM FOR COMPUTING THE FLOW ABOUT WING-PYLON/NACELLE COMBINATIONS-Reference-Cited by-同舟云学术

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A TRANSONIC MUTUAL INTERFERENCE PROGRAM FOR COMPUTING THE FLOW ABOUT WING-PYLON/NACELLE COMBINATIONS

Published:1980-07-14 Issue: Volume: Page:
ISSN:
Container-title:13th Fluid and PlasmaDynamics Conference
language:
Short-container-title:

Author:

SRAKOWSKI A.J.¹,SHREWSBURY G.D.¹,LORES M.E.¹

Affiliation:

1. LOCKHEED-GEORGIA COMPANY, MARIETTA, GA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1980-1333

Reference11 articles.

1. Sokney, J. S.: symmetric inlets Including Rotational Flow Effects," AiAA Paper 80-0341. "Transonic Flow Around Axi

2. Reynher, T. A.: rlTransonic Patentiai Flow Around Axisymnetric inlets and Bodies at Angle of Attack," AiAA Paper 77-145.

3. Boppe C. W.; and Stern, M. A. "Simulated Transonic Flows far Aircraft with Nacelles, Pylons, and Winglets," AiAA Paper 80-0130.

4. aclions," AIAA Paper 80-0127.

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. 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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