Enhancement of the leading-edge separation vortices by trailing-edge lateral blowing
Author:
Affiliation:
1. University of Tokyo, Tokyo 113, Japan
2. Institute for Space and Astronautical Science, Kanagawa 229, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13330
Reference10 articles.
1. A Conceptual Study of Leading-Edge-Vortex Enhancement by Blowing
2. Navier Stokes computation of the flow field over delta wings with spanwise leading edge blowing
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1. Aerodynamics and Vortex Flowfield of a Slender Delta Wing With Apex Flap and Tip Flap;Journal of Fluids Engineering;2017-03-20
2. Water Tunnel Experimental Studies of Leading Edge Vortex Control on Delta Wing MAV;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
3. Effect of Lateral Blowing for Flat Delta Wings with Various Planforms and a Rectangular Wing;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2007
4. Aerodynamic performance enhancement by lateral blowing for reusable launch vehicles;57th International Astronautical Congress;2006-10-02
5. Lift Augmentation by Lateral Blowing for RLVs with Various Fuselage-Cross Sections;3rd AIAA Flow Control Conference;2006-06-05
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