A unique measurement technique to study laminar-separation bubble characteristics on an airfoil
- 8 June 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
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- Design and wind tunnel test of a high performance low Reynolds number airfoilPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
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- Determination of mean and dynamic skin friction, separation and transition in low-speed flow with a thin-film heated elementJournal of Fluid Mechanics, 1966