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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Comparison of performance of four side mounted inlets over Mach number range of 0.88 to 2.2 and angle of attack to 14 degrees
Aerodynamic loads on external store adjacent to 60 deg delta wing at Mach numbers 0.75 to 1.96
Mach number and air temperature effect on hypersonic flow over blunt bodies
Turbulent skin friction at high Reynolds number and low supersonic speeds
Impact pressure probe response characteristics in high speed flows with transition Knudsen numbers
Maximum model-size determination and effect of sting diameter on entry shape and sphere for low Mach number testing - Apollo spacecraft wind tunnel tests
Turbulent boundary layer on hollow cylinder at Mach 6, high Reynolds number, and zero heat transfer
Pressure distribution and flow fields of blunted cones at hypersonic Mach numbers
Random numbers generated by linear recurrence modulo 2 and correlation and distribution functions
Longitudinal stability and control characteristic of M wing aircraft at various Mach numbers
Modulo-two linear recurrence technique for generating sequences of apparently random numbers that have certain regularities
Franck-Condon factors computed to highest known vibrational quantum numbers for NO band system
Franck-Condon factors computed and tabulated to high vibrational quantum numbers for molecular oxygen band system
Wind tunnel studies of six cones for pressure probes to determine Mach number, total pressure and flow angles
Aerodynamic characteristics of spherically blunted cones at Mach numbers from 0.5 to 5.0
Drag characteristics of low drag bodies of revolution at Mach numbers from 0.6 to 4.0
Impact pressure probe response characteristics in free-molecular and continuum flows with transition Knudsen numbers
Measured and calculated flow conditions on forward fuselage of X-15 plane and model at Mach numbers from 3.0 to 8.0