Prediction of vortex breakdown in leading edge vortices above slender delta wings-Reference-Cited by-同舟云学术

Prediction of vortex breakdown in leading edge vortices above slender delta wings

Published:1998-06-15 Issue: Volume: Page:
ISSN:
Container-title:2nd AIAA, Theoretical Fluid Mechanics Meeting
language:
Short-container-title:

Author:

Rusak Zvi¹,Lamb David¹

Affiliation:

1. Rensselaer Polytechnic Inst., Troy, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-2860

Reference55 articles.

1. High Angle of Attack Aerodynamics

2. Peckham, D.H. and Atkinson. S.A.''Preliminary Results of Low Speed Wind Tunnel Tests on a Gothic Wing of Aspect Ratio 1.0." Aeronautical Research Council, CP508, 1957.

3. Lambourne, N.C. and Bryer. D.W. "TheBurstingofLeading-Edge Vortices-Some Observations and Discussion of the Phenomenon," Aeronautical Research Council, Reportsand Memoranda R & M No. 3282. pp.1-36,1962.

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