Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊

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