Results 261 to 270 of about 47,524 (305)

Tangential slot injection in supersonic flow.

AIAA Journal, 1967
The flowfield associated with tangential slot injection of a gas into a supersonic external stream is of current technological and academic interest. The present study can be divided into three areas. First, detailed profiles in the near flowfield were determined with an interferometer for air injection into a Mach 2.1 airstream past a flat plate ...
H. GILREATH, J. SCHETZ
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Supersonic Flow and Shocks

2019
The present chapter treats supersonic flows and shock fronts (also termed shock waves or simply shocks). A shock is an enduring and smooth surface in a fluid through which the fluid passes; in this passage, the fluid density, pressure, velocity, and temperature all undergo abrupt changes (‘jumps’).
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Vortical solutions in supersonic corner flows

31st Aerospace Sciences Meeting, 1993
Vortical solutions are investigated for inviscid supersonic steady flows, described by the steady-state Euler equations, that occur in the corner region generated by two orthogonal ramps. Complex shock interactions appear, with the formation of a vorticity field in the corner region and the vorticity itself converging into spiral singularities ...
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On wing–body interference in supersonic flow

Mathematika, 1966
Although the theory of supersonic inviscid flow past thin wings and slender bodies has received an enormous amount of attention in recent years, comparatively little attention has been paid to the interaction between wings and finite bodies. The principal reason stems from the extensive numerical work that has to be done in order to form a detailed ...
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Supersonic Flow With Variable Specific Heat

Journal of Applied Mechanics, 1952
Abstract Formulas are developed for stagnation conditions and one-dimensional flow through shock waves, including Rankine-Hugoniot values, taking into account the variation of the specific heat of air with temperature by means of the concept of mean specific heats.
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On Supersonic Flow Past Thick Airfoils

Journal of the Aerospace Sciences, 1960
= = = = = — speed of sound, in units of limiting velocity pressure coefficient airfoil profile undisturbed-flow Mach number pressure gas constant entropy temperature Cartesian coordinates velocity components in x and y directions, in units of limiting velocity velocity, in units of limiting velocity ratio of specific heats flow inclination to ...
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Supersonic Beams, Supersonic Flow

2023
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A conservative and consistent scalar filtered mass density function method for supersonic flows

Physics of Fluids, 2021
Lin Zhang, Jianhan Liang, Mingbo Sun
exaly  

Physics-informed neural networks for inverse problems in supersonic flows

Journal of Computational Physics, 2022
Ameya D Jagtap, Zhiping Mao, Nikolaus A Adams   +2 more
exaly  

An eigendecomposition approach to turbulence production in supersonic streamwise vortex dominated flows

Physics of Fluids, 2021
Davide Vigano
exaly