The research on active flow control method with vibration diaphragm on a NACA0012 airfoil at different stalled angles of attack
Author:
Funder
National Natural Science Foundation of China
Shanghai Science and Technology Commission
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference10 articles.
1. Active Flow Control Technology;Kral,2000
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3. Effects of synthetic jet actuation on a ramping NACA 0015 airfoil;Traub;J. Aircr.,2004
4. Turbine blade boundary layer separation suppression via synthetic jet: an experimental and numerical study;Bernardini;Int. J. Therm. Sci.,2012
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