Flight Tests of an Airplane Model with a 62 Degree Swept-back Wing in the Langley Free-flight Tunnel
Low-Speed Static and Dynamic Force Tests of a Generic Supersonic Cruise Fighter Configuration
Design Issues Associated with Full-Scale Application of Active Control of Vortex Flows
Suppression of Pilot-Induced Oscillation (PIO)
Eighth Space Cryogenic Workshop, 31 July-1 Aug. 1989, Pasadena, CA, USA