Comment on 'Aeroelastic oscillations caused by transitional boundarylayers and their attenuation'
Author:
Affiliation:
1. Lockheed Missiles & Space Company, Sunnyvale, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45690
Reference10 articles.
1. Fluid dynamics of airfoils with moving surface boundary-layer control
2. 2Mokhtarian, F. "Fluid Dynamics of Airfoils with Moving Surface Boundary-Layer Control," Ph.D. Thesis,University of British Columbia, Vancouver, Canada, Feb. 1988.
3. Effect of moving surfaces on the airfoil boundary-layer control
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1. Self-sustained aeroelastic oscillations of a NACA0012 airfoil at low-to-moderate Reynolds numbers;Journal of Fluids and Structures;2008-07
2. Reply by Author to D. G. Mabey and P. R. Ashill;Journal of Aircraft;1992-05
3. Comment on 'Transition effects on airfoil dynamics and implications for subscale tests';Journal of Aircraft;1992-05
4. Transition effects on airfoil dynamics and the implications for subscale tests;Journal of Aircraft;1989-12
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