NASA STI Repository (National Aeronautics and Space Administration) · 1959 · 79 citations · 2 references
Open access
EngineeringAerospace EngineeringPhysicsAerodynamicsComputational Fluid DynamicsFluid DynamicsComputational AerodynamicsSupersonic AerodynamicsMach NumberSupersonic Flow
Some 100 numerical computations have been carried out for unyawed bodies of revolution with detached bow waves. The gas is assumed perfect with gamma = 5/3, 7/5, or 1. Free-stream Mach numbers are taken as 1.2, 1.5, 2, 3, 4, 6, 10, and infinity. The results are summarized with emphasis on the sphere and paraboloid.
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Formulae for Numerical Differentiation
W. G. Bickley · The Mathematical Gazette · 1941 · 130 citations