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Application of Some Lifting-Body Reentry Concepts to Missile Design
Development of Micro Air Vehicle Technology With In-Flight Adaptive-Wing Structure
Mission Adaptive Wing Soars at NASA Facility
Experimental Investigation of Leading-Edge Thrust at Supersonic Speeds
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
Estimated Benefits of Variable-Geometry Wing Camber Control for Transport Aircraft