1-11 of 11 Books
Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration
Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration
By F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration (1992 Edwards, Calif.)
Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
By Scott P. Fears
Computation of three-dimensional compressible boundary-layers to fourth-order accuracy on wings and fuselages
Computation of three-dimensional compressible boundary-layers to fourth-order accuracy on wings and fuselages
By Venkit Iyer
Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
By Ken Craig
Static aeroelastic analysis of a three-dimensional generic wing
Static aeroelastic analysis of a three-dimensional generic wing
By John A. Green
Image processing of aerodynamic data
Image processing of aerodynamic data
By Nettie D. Faulcon
Water tunnel flow visualization study through poststall of 12 novel planform shapes
Water tunnel flow visualization study through poststall of 12 novel planform shapes
By Gregory M. Gatlin
Additional development of the XTRAN3S computer program
Additional development of the XTRAN3S computer program
By Christopher J. Borland
Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
By Robert Alan Hess
Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
By John E. Lamar