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General Discussion: Supersonic Flows
1983We must now try to draw conclusions on the papers which were presented. I invite the participants to make their remarks, criticisms and suggestions. I first propose to review and classify the topics, to examine the experimental methods, to make a survey of the main results which were obtained, and finally to compare prediction with experiment.
R. Dumas, L. Fulachier
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Spectral Simulation of Supersonic Reactive Flows
SIAM Journal on Numerical Analysis, 1998The authors present a Chebyshev collocation scheme for the numerical simulation of reactive flows with shock waves. It is shown that spectral methods are suitable for the numerical approximation of reactive flows interacting with shock waves. Theoretical and numerical results on interactions of hydrogen jets with shock waves are analyzed, and ...
Don, Wai Sun, Gottlieb, David
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Supersonic wake flow visualization
AIAA Journal, 1969Supersonic wake flow visualization, obtaining direct photographs of various smoke ...
C. HALL, JR., T. MUELLER, W. SULE
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Leeward Separated Supersonic Flows
1991Using various experimental methods the “architecture” of the separated flows formed at the lee-side of a blunt cone and delta wing is investigated. The flow structure evolution during the variation of the angle of attack and the Mach number is discussed.
V. Ya. Borovoi +2 more
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2010
Compressible flow past thin wings and slender bodies are studied. First, subsonic flow past thin wings are analyzed by means of potential flow theory. The kernel function method is introduced for arbitrary planforms undergoing simple harmonic oscillations.
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Compressible flow past thin wings and slender bodies are studied. First, subsonic flow past thin wings are analyzed by means of potential flow theory. The kernel function method is introduced for arbitrary planforms undergoing simple harmonic oscillations.
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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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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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Assessment methods and performance metrics for redox flow batteries
Nature Energy, 2021Yang Shi, Yi-Chun Lu
exaly

