Two-dimensional computational analysis of a transport high-lift system and a comparison with flight-test results
Author:
Affiliation:
1. Lockheed Engineering & Sciences Co.; NASA, Langley Research Center, Hampton, VA
2. CaliforniaUniv., Davis
3. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-3533
Reference28 articles.
1. IDillner, B., May, F.W., and McMasters, J.H. "Aerodynamic Issues in the Design of High-LiftSystemsforTransport Aircrafi;', AGGD CP-365. May 1984.
2. 4White, J.J. "Advanced Transport Operating Systems Program,'' SAE Paper 901969, October,1990.
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1. Design methodology for high-lift systems on subsonic transport aircraft;6th Symposium on Multidisciplinary Analysis and Optimization;1996-08-22
2. In-Flight pressure measurements on a subsonic transport high-lift wing section;Journal of Aircraft;1995-05
3. Viscous-flow analysis of a subsonic transport high-lift system including comparisons with flight-measured results;33rd Aerospace Sciences Meeting and Exhibit;1995-01-09
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