Predicting optimal drooped leading-edge extension length for an NACA 0015 wing through flow visualization
Asay, August A. Snyder, Melvin H.
Asay, August A.
Snyder, Melvin H.
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1988
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Keywords
Leading edges (Aerodynamics),Flow visualization,Aerofoils,Stalling (Aerodynamics)
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Citation
Asay, August A., and Melvin H. Snyder. Predicting Optimal Drooped Leading-Edge Extension Length for an NACA 0015 Wing through Flow Visualization. Institute for Aviation Research, Wichita State University, 1988.
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Cover title.;"This project was supported, in part, by the Federal Aviation Administration through contract no. DT FA 03-86-C-0041."
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Institute for Aviation Research, Wichita State University
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IAR (series)