Boundary-Layer Control by Means of Pulsed Jets at Different Inclination Angles
Author:
Affiliation:
1. Technical University of Berlin, 10587 Berlin, Germany
Funder
Deutsche Forschungsgemeinschaft
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060474
Reference51 articles.
1. INTRODUCTION TO SHOCK-INDUCED SEPARATION AND ITS PREVENTION BY DESIGN AND BOUNDARY LAYER CONTROL
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4. Actuators for Active Flow Control
5. Vortical structure in the wake of a transverse jet
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