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Shock Effects on Delta Wing Vortex Breakdown

Published:2009-05 Issue:3 Volume:46 Page:903-914
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Schiavetta L. A.¹,Boelens O. J.²,Crippa S.³,Cummings R. M.⁴,Fritz W.⁵,Badcock K. J.⁶

Affiliation:

1. University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom

2. National Aerospace Laboratory, NLR, 1006 BM Amsterdam, The Netherlands

3. Royal Institute of Technology, 100 44 Stockholm, Sweden

4. U.S. Air Force Academy, USAFA Colorado 80840

5. EADS Military Air Systems, 81633 Munich, Germany

6. University of Liverpool, Liverpool, England L69 7BZ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.38792

Reference24 articles.

1. Vortex breakdown location over 65° delta wings empiricism and experiment

2. Compressible inviscid vortex flow of a sharp edge delta wing

3. Surface Reflective Visualizations of Shock-Wave/Vortex Interactions Above a Delta Wing

Cited by 25 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. Physical aspects of vortex-shock dynamics in delta wing configurations;Physics of Fluids;2024-06-01

2. Prediction of concentrated vortex aerodynamics: Current CFD capability survey;Progress in Aerospace Sciences;2024-05

3. Towards the understanding of vortex breakdown for improved RANS turbulence modeling;Aerospace Science and Technology;2024-03

4. Turbulence Model Effects on Vortex Interaction Prediction on a Multiswept Delta Wing;Journal of Aircraft;2023-09-13

5. Experimental and numerical analysis of the aerodynamics and vortex interactions on multi-swept delta wings;CEAS Aeronautical Journal;2023-08-26

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