Weissinger's model of the nonlinear lifting-line method for aircraft design
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-597
Reference16 articles.
1. Carlson,H.W.,Darden, C.M.,andMann,M.J. "Validation of aComputerCodeforAnalysis of SubsonicAerodynamicPerformance ofWingsWith FlapsinCombinationWith aCanard orHorizontal Tail andanApplication toOptimization,"NASATP 2961,January 1990.
2. Numerical lifting line theory applied to drooped leading-edge wings below and above stall
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