Effect of Plasma Actuator Excitation for Controlling Bypass Transition in Boundary Layers
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
2010-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
EFFECT OF PLASMA ACTUATOR EXCITATION FOR CONTROLLING BYPASS TRANSITION IN BOUNDARY LAYERS
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|A Bypass Transition Model for Boundary Layers (93-GT-90)
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|Bypass Transition in Boundary Layers Including Curvature and Favorable Pressure Gradient Effects
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