Parametric Study and Effect of Nose-Piece Attachment on Sonic Boom Mitigation-Reference-Cited by-同舟云学术

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Parametric Study and Effect of Nose-Piece Attachment on Sonic Boom Mitigation

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Ozcer Isik¹,Kandil Osama¹,Yagiz Bedri¹

Affiliation:

1. Old Dominion University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1243

Reference9 articles.

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. Design Optimization of Nose Geometry of F-5E Aircraft for Sonic Boom Mitigation;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

2. Optimization of Delta Wing Geometry Parameters for Sonic Boom Mitigation;37th AIAA Fluid Dynamics Conference and Exhibit;2007-06-15

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