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Experimental Investigations to Fully Map The Flow Field Around A Wind Tunnel Model of A Transport Airplane
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English
Abstract
A description of the results of research conducted to fully map the three-dimensional flow field associated with a typical transport airplane. Details of the method employed to map the flow field, pictures of the longitudinal development of fore body vortices, and a comparison of the experimental results with empirical methods are presented. The results also include a graphic description of the wake propagation behind deflected spoiler panels.
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Citation
Stremel, P., "Experimental Investigations to Fully Map The Flow Field Around A Wind Tunnel Model of A Transport Airplane," SAE Technical Paper 800630, 1980, https://doi.org/10.4271/800630.Also In
References
- Mack, M.D. Seetharam, H.C. Kuhn, W.G. Bright, J.T. Aerodynamics of Spoiler Control Devices AIAA Paper No. 79-1873 August 1979
- Seetharam, H.C. Wentz, W.H., Jr. Experimental Studies of Flow Separation and Stalling of a Two-Dimensional Airfoil at Low Speeds July 1975
- Seetharam, H.C. Wentz, W.H., Jr. A Low Speed Two-Dimensional Study of Flow Separation on the GA(W)-I Airfoil with 30 Percent Chord Fowler Flap May 1977
- USAF DATCOM y