Computational Simulation and PIV Measurements of the Laminar Vortical Flowfield for a Delta Wing at High Angle of Attack-Reference-Cited by-同舟云学术

Computational Simulation and PIV Measurements of the Laminar Vortical Flowfield for a Delta Wing at High Angle of Attack

Published:2003-01-06 Issue: Volume: Page:
ISSN:
Container-title:41st Aerospace Sciences Meeting and Exhibit
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Author:

Cummings Russell¹,Morton Scott¹,Siegel Stefan¹

Affiliation:

1. U.S. Air Force Academy

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1102

Reference24 articles.

1. Numerical investigation of high incidence flow over a double-delta wing

2. Computational investigation of slot blowing for fuselage forebody flow control

3. Huang,X.Z.,Lui, T.C., andHanff,E.S. "A NovelConceptforControlling Leading-EdgeVortex Breakdown andRelated PreliminaryWater Tunnel Experiment," AIAAPaper2001-4143,Aug.2001.

4. Research into vortex breakdown control

5. Oscillation of Vortex Breakdown Location and Blowing Control of Time-Averaged Location

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