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


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    Title :

    Extending Swept-Wing Natural Laminar Flow Using Discrete Roughness Element


    Contributors:
    Mujeeb Malik (author) / P. Balakumar (author) / Fei Li (author) / Meelan Choudhari (author)

    Conference:

    41st AIAA Fluid Dynamics Conference ; 2011 ; Honolulu, HI, US


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English







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