The influence of laminar separation and transition on low Reynolds number airfoil hysteresis
- 1 September 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (9) , 763-770
- https://doi.org/10.2514/3.45199
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Boundary layer characteristics of the Miley airfoil at low Reynolds numbersJournal of Aircraft, 1984
- Boundary layer characteristics of the Miley airfoil at low Reynolds numbersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- The influence of free-stream disturbances on low Reynolds number airfoil experimentsExperiments in Fluids, 1983
- Experimental Studies of Separation on a Two-Dimensional Airfoil at Low Reynolds NumbersAIAA Journal, 1982
- AERODYNAMIC MEASUREMENTS AT LOW REYNOLDS NUMBERSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Gossamer Condor and Albatross: A Case Study in Aircraft DesignPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980