1-17 of 17 Books
Shock-tunnel combustor testing for hypersonic vehicles
Shock-tunnel combustor testing for hypersonic vehicles
By Mark Loomis
Development of advanced methods of trajectory and structural analysis for hypersonic aircraft
Development of advanced methods of trajectory and structural analysis for hypersonic aircraft
By Mark D. Ardema
Experimental aerothermodynamic research of hypersonic aircraft
Experimental aerothermodynamic research of hypersonic aircraft
By Joseph W. Cleary
Numerical modeling of a cryogenic fluid within a fuel tank
Numerical modeling of a cryogenic fluid within a fuel tank
By Donald S. Greer
Materials research for high speed civil transport and generic hypersonics
Materials research for high speed civil transport and generic hypersonics
By Paul Schulz
Assessment of NASA's aircraft noise prediction capability
Assessment of NASA's aircraft noise prediction capability
By Milo D. Dahl
NASA-UVa light aerospace alloy and structures technology program supplement: aluminum-based materials for high speed aircraft: semi-annual report, July 1, 1992-December 31, 1992
NASA-UVa light aerospace alloy and structures technology program supplement: aluminum-based materials for high speed aircraft: semi-annual report, July 1, 1992-December 31, 1992
By E. A. Starke
On waverider shapes applied to aero-space plane forebody configurations
On waverider shapes applied to aero-space plane forebody configurations
By Maurice L. Rasmussen
Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature
Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature
By Lawrence F. Reardon
Propulsion system integration for Mach 4 to 6 vehicles
Propulsion system integration for Mach 4 to 6 vehicles
By Victor Salemann
Hypersonic transport preliminary performance estimates for an all-body configuration
Hypersonic transport preliminary performance estimates for an all-body configuration
By Thomas J. Gregory
A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept
A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept
By Bandu N. Pamadi
Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5
Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5
By Christopher E. Glass
Trajectory optimization and guidance law development for national aerospace plane applications
Trajectory optimization and guidance law development for national aerospace plane applications
By Anthony J. Calise
Airbreathing hypersonic systems focus at NASA Langley Research Center
Airbreathing hypersonic systems focus at NASA Langley Research Center
By James L. Hunt
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
By Jim A. Penland
Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation
Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation
By William L. Ko