Surface flow topology on a delta wing at high incidence for a range of roll angles-Reference-Cited by-同舟云学术

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Surface flow topology on a delta wing at high incidence for a range of roll angles

Published:1996-06-17 Issue: Volume: Page:
ISSN:
Container-title:14th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Huang X.¹,Hanff E.¹,Jobe Charles²

Affiliation:

1. National Research Council of Canada, Inst. for Aerospace Research, Ottawa

2. USAF, Wright Lab., Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2398

Cited by 7 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. Effect of Sideslip on High-Angle-of-Attack Vortex Flow over Close-Coupled Canard Configuration;Journal of Aircraft;2016-01

2. Skin friction fields on delta wings;Experiments in Fluids;2009-05-29

3. NATO RTO AVT Task Group-080 "Vortex Breakdown over Slender Wings": Objectives and Overview;21st AIAA Applied Aerodynamics Conference;2003-06-21

4. Wind-Tunnel Study on a 65-deg Delta Wing at Sideslip;Journal of Aircraft;2003-03

5. Effects of Sideslip on the Characteristics of a 65-deg Delta Wing;41st Aerospace Sciences Meeting and Exhibit;2003-01-06

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