A method for estimating the propulsion induced aerodynamic characteristics of STOL aircraft in ground effect
Author:
Affiliation:
1. Rockwell International Corp., Columbus, OH
2. U.S. Naval Material Command, Naval Air Development Center, Warminster, PA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-169
Reference10 articles.
1. Effect, Interim NADC Report NADC 80226-60,>"".
2. Berg, A.; Longitudinal Splitting o f A Wind Tunnel Moving Ground Belt and I t s Effect on a Jet Flap Model, UTIAS TN 4173, AD 904401, Jan. 1972.
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3. A correlation of the effects of the ground vortex on the aerodynamic characteristics of a generic STOL aircraft configuration;International Powered Lift Conference;1993-08-22
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