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Shock-tunnel combustor testing for hypersonic vehicles
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Numerical modeling of a cryogenic fluid within a fuel tank
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Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5
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Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature
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Experimental aerothermodynamic research of hypersonic aircraft
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Development of advanced methods of trajectory and structural analysis for hypersonic aircraft
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Airbreathing hypersonic systems focus at NASA Langley Research Center
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Materials research for high speed civil transport and generic hypersonics
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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
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On waverider shapes applied to aero-space plane forebody configurations
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Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation
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Hypersonic transport preliminary performance estimates for an all-body configuration
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Assessment of NASA's aircraft noise prediction capability
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A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept
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Propulsion system integration for Mach 4 to 6 vehicles
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Trajectory optimization and guidance law development for national aerospace plane applications
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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
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