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Investigation of the validity of Reynolds averaged turbulence models at the frequencies that occur in turbomachinery by Kuhn, Gary D.
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Postflight aerothermodynamic analysis of Pegasus[copyright] using computational fluid dynamic techniques by Kuhn, Gary D.
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3
Theoretical study of vortex shedding from bodies of revolution undergoing coning motion / by Kuhn, Gary D.
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4
Calculation of compressible, nonadiabatic boundary layers in laminar, transitional and turbulent flow by the method of integral relations / by Kuhn, Gary D.
Published 1971Call Number: Loading…Search for the full-text version of this title in HathiTrust
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5
Calculation of compressible turbulent boundary layers with pressure gradients and heat transfer / by Lynes, Larry L.
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Related Subjects
Heat transfer
Mathematical models
Turbulence
Turbulent boundary layer
Ablative materials
Aerothermodynamics
Air flow
Axisymmetric flow
Bodies of revolution
Boundary layer
Compressible boundary layer
Computational fluid dynamics
Computer programs
Computer systems performance
Cones
Configurations
Equations of motion
Flight tests
Flow distortion
Fluid dynamics
Heat
Hypersonic speed
Momentum
Postflight analysis
Pressure distribution
Pressure gradients
Reynolds number
Shock waves
Slender bodies
Thermal protection