New, accurate, vectorized approximations of state surfaces for the thermodynamic and trans- port properties of equilibrium air
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1
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Computational fluid dynamics validation using surface heat transfer measurements of hypersonic flowfields
American Institute of Aeronautics and Astronautics |
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CALCULATION OF HYPERSONIC NON-EQUILIBRIUM VISCOUS FLOW USING SECOND ORDER BOUNDARY LAYER THEORY
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Computer codes for the evaluation of thermodynamic and transport properties for equilibrium air to 30000 K
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Calculations and curve fits of thermodynamic and transport properties for equilibrium air to 30000 K
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |