The Design and Test of a Swept Wing Upper Surface Blowing Concept-Reference-Cited by-同舟云学术

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The Design and Test of a Swept Wing Upper Surface Blowing Concept

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Harrison Neal¹,Vassberg John¹,Dehaan Mark¹,Gea Lie-Mine¹

Affiliation:

1. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1102

Reference16 articles.

1. C-17transports KillerWhaleKeiko,URL:http://en.wikipedia.org/wiki/Keiko_%28orca%29,January1996.

2. SpeedAgileBroadAgencyAnnoucement.BAA-07-07-PKVSACD

3. fuselage,wing,empennage,and exhaust flowcontroldevices",Patent No.US8,061,655,filed 22Nov.2011.

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. Coupling Effects on Distributed Multi-Propeller Channel Wing at Low Speed Condition;Energies;2022-07-23

2. Enhancements to the FAST-MAC Circulation Control Model and Recent High-Reynolds Number Testing in the National Transonic Facility;31st AIAA Applied Aerodynamics Conference;2013-06-22

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