Supersonic Aerodynamic Characteristics of Some Reentry Concepts for Angles of Attack to 90 Deg
Wind Tunnel Tests on an Outer Wing Segment of the ASW-19X Sailplane
Measured and Predicted Pressure Distributions on the AFTI/F-111 Mission Adaptive Wing
Study of Supersonic Wings Employing the Attainable Leading-Edge Thrust Concept
High-Speed Investigation of Low-Drag Wing Inlets
Flight Test of an Adaptive Configuration Optimization System for Transport Aircraft
Estimated Benefits of Variable-Geometry Wing Camber Control for Transport Aircraft