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Experimental Transonic Flutter Characteristics of Two 72 Deg-Sweep delta-Wing Models
Application of Some Lifting-Body Reentry Concepts to Missile Design
Development of Control Systems for Space Shuttle Vehicles. Volume 2 Appendixes
The delta and Thor/ Agena Launch Vehicles for Scientific and Applications Satellites
Lift-to-Drag Ratios of Semispan delta Wing Configurations at Supersonic and Hypersonic Mach Numbers
Ground Effects Related to Landing of Airplanes with Low-Aspect-Ratio Wings
Pressure Measurements on a Slender Rhombic Cone at Incidence at Mach Numbers from 0.4 to 1.1
Supersonic Aerodynamic Characteristics of an Advanced F-16 Derivative Aircraft Configuration
Space Shuttle Aerodynamic Characteristics of the Nr delta Wing Orbiter, M Equals 0.6 to 1.3
Wind-Tunnel Investigation at a Mach Number of 1.53 of an Airplane with a Triangular Wing
Low-Speed Wind-Tunnel Measurements of Surface Pressure Fluctuations on Two Slender-Wing Models
Comparison of Platforms for the Aerial Exploration of Titan
Aerodynamic Control of NASP-Type Vehicles through Vortex Manipulation, Volume 4
Delta- a Scientific and Application Satellite Launch Vehicle
Canadian Communication Satellite/Delta Launch (TELESAT-B) (ANIK II)
Thrust-Induced Effects on a Pitching-Up Delta Wing Flow Field: Control of Stalled Wings
Calculation of Aerodynamic Characteristics of Wing and Fuselage in Supersonic Flow
Pressure Distribution on a Hypersonic delta Wing of Diamond Cross-Section