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by Daniel W. Banks
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High-lift systems on commercial subsonic airliners
Peter K. C. Rudolph
Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
Scott P. Fears
Wing pressure distributions from subsonic tests of a high-wing transport model
Zachary T. Applin
Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
Bruce Charles
Lift increase obtained with boundary layer suction on a 10% double wedge airfoil with a 20% chord leading and trailing edge flaps
Harold William Davidson
Active Spanwise Lift Control
Joaquim Neto Dias
Application of particle image velocimetry to a study of flow about a multi-element airfoil
Stephen M. Walker
Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap
Ahmed Hassan
