Outline - Motivation - Transition control using discrete roughness elements (DRE) - Subsonic Aircraft Roughness Glove Experiment (SARGE) - Crossflow transition in the absence of control - Effect of control - Concluding Remarks
Extending Swept-Wing Natural Laminar Flow Using Discrete Roughness Element
41st AIAA Fluid Dynamics Conference ; 2011 ; Honolulu, HI, US
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Englisch
Discrete-Roughness-Element-Enhanced Swept-Wing Natural Laminar Flow at High Reynolds Numbers
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