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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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Helium flow at hypersonic speed used to calculate hypersonic flutter data on low aspect ratio, flexible, wing-fuselage configuration
Coupling between inviscid and viscid flows in hypersonic stagnation region investigated at high flight velocities with significant radiative heat transfer
Measured and calculated flow conditions on forward fuselage of X-15 plane and model at Mach numbers from 3.0 to 8.0
Pressure distributions and aerodynamic characteristics of Nimbus B fuel capsule in hypersonic flow
Effect of two dimensional multiple sine wave protrusions on pressure and heat transfer distributions for flat plate in hypersonic flow
Interference effects of canard controls on longitudinal aerodynamic characteristics of winged body in hypersonic flow
Effect of radiative heat transfer in low Reynolds number hypersonic flow about blunt body
Compressible laminar boundary layer equations considered for hypersonic flow around slender bodies
Apollo Command Module aerodynamics at reentry altitudes simulated by models in hypersonic flow
Nonsimilar compressible laminar boundary layer equations for hypersonic flow around slender bodies solved by integration based on steepest descent method
Aerodynamic measurements on Apollo CM model at hypersonic flow simulating earth orbital reentry trajectory
Radiative transfer effects in low Reynolds number or merged layer regime of hypersonic flow about axisymmetric blunt bodies, including thin shock layer theory
Radiation equilibrium temperature measured downstream of transpiration cooled gas flow near slender cone vertex in continuous flow hypersonic tunnel
Aerodynamic interference effects on half-cone bodies with thin wings in hypersonic flow
Heat transfer measurements on flat plate with trailing edge flap in hypersonic flow
Pressure distribution of spherically-blunted 60 deg half-angle cone in hypersonic flow
Shock wave shapes over axisymmetric power law bodies in hypersonic flow, noting asymptotic flow theory implications
Viscous shock layer equations of laminar hypersonic flow past blunt body at moderate to high Reynolds numbers