Transition behavior on flat plate delta wings-Reference-Cited by-同舟云学术

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Transition behavior on flat plate delta wings

Published:1994-06-20 Issue: Volume: Page:
ISSN:
Container-title:12th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Visser Kenneth¹,Washburn Anthony²

Affiliation:

1. National Research Council, Hampton, VA

2. Vigyan, Inc., Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-1850

Reference15 articles.

1. Earnshaw, P.B. and Lawford, J.A. "Low Speed Wind Tunnel Experiments on a Series of Sharp Edged Delta Wings"ARC R &M, No 3424,March 1964.

2. Lemaire, D. A. "Some Observations of theLow-Speed Flow Over a Sharp-Edged Delta Wing of Unit Aspect Ratio,AeronauticalResearchLaboratoriesAero.Report 126,January 1965.

Cited by 4 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. Performance of Transition-Sensitive Models in Predicting Flow Structures over Delta Wings;Journal of Aircraft;2015-01

2. Physical Considerations of Leading Edge Flows;22nd Applied Aerodynamics Conference and Exhibit;2004-06-20

3. Vortex breakdown location over 65-deg delta wings - Empiricism and experiment;16th AIAA Applied Aerodynamics Conference;1998-06-15

4. Tunnel wall effect on the flow around a 76/40-deg double-delta wing;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12

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