Suction and Pulsed-Blowing Flow Control Applied to an Axisymmetric Body-Reference-Cited by-同舟云学术

Suction and Pulsed-Blowing Flow Control Applied to an Axisymmetric Body

Published:2013-10 Issue:10 Volume:51 Page:2432-2446
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Wilson Jacob¹,Schatzman David²,Arad Eran³,Seifert Avraham⁴,Shtendel Tom⁴

Affiliation:

1. Development & Engineering Center Research, Development and Engineering Command, NASA Ames Research Center, Moffett Field, California 94035

2. Development & Engineering Center Research, Development and Engineering Command, Science and Technology Corporation, Moffett Field, California 94035

3. Computational Fluid Dynamics, Aeronautical Systems, Rafael Ltd., 31021 Haifa, Israel

4. School of Mechanical Engineering, Tel Aviv University, 69978 Tel Aviv, Israel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052333

Reference27 articles.

1. also “Motion of Fluids with Very Little Viscosity,” NACA TM-452, March 1928.

2. GlauertM. B. “The Design of Suction Aerofoils with a Very Large CL-Range,” Aeronautical Research Council, Rept. 2111, Nov. 1945.

3. GlauertM. B.WalkerW. S.RaymerW. G.GregoryN. “Wind-Tunnel Tests on a Thick Suction Aerofoil with a Single Slot,” Aeronautical Research Council, Rept. 2646, Oct. 1948.

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