Results 11 to 20 of about 5,113,406 (258)
Rate Effects in Hypersonic Flows
Hypersonic flows are energetic and result in regions of high temperature, causing internal energy excitation, chemical reactions, ionization, and gas-surface interactions.
G. Candler
semanticscholar +3 more sources
Magnetohydrodynamic Control of Hypersonic Separation Flows
Magnetohydrodynamic (MHD) control of hypersonic laminar separation flows is investigated in this paper. A series of numerical simulations over various geometry configurations, namely, a compression corner and a double wedge ramp hypersonic inlet, have ...
Shichao Luo +3 more
doaj +1 more source
Transitional flow has a significant impact on vehicles operating at supersonic and hypersonic speeds. An economic way to simulate this problem is to use computational fluid dynamics (CFD) codes.
Yu Chen, Nick Gibbons
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Correction to: High-enthalpy hypersonic flows
An amendment to this paper has been published and can be accessed via the original article.
Joseph J. S. Shang, Hong Yan
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MSAT: Matrix stability analysis tool for shock-capturing schemes
The simulation of supersonic or hypersonic flows often suffers from numerical shock instabilities if the flow field contains strong shocks, limiting the further application of shock-capturing schemes.
Weijie Ren +4 more
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The rotational energy of diatomic gases would be activated by the process of intermolecular collisions in high-temperature hypersonic flows. In this paper, a multi-temperature nonlinear coupled constitutive model has been proposed for simulating the ...
Zhenyu Yuan +3 more
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Black-box optimization methods for hypersonic flow problems [PDF]
This review examines the application of black-box optimization methods to hypersonic flow problems, with a particular emphasis on scenarios where computational fluid dynamics (CFD) simulations function as opaque, nontransparent models.
Davood Hoseinzade +2 more
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An efficient method to predict thermal loads on hypersonic vehicles in rarefied flows is immediately needed, especially when designing the thermal protection system.
Dongming Ding +4 more
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Design of hypersonic wavecatcher intake at Mach 12 with rectangular-to-elliptical shape transition
Wavecatcher (inward-turning) intake flows, at design Mach 12, are investigated numerically, to display the effect of wall temperature on flow structures and intake performance.
Feng-Yuan Zuo, Sannu Mölder
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Oblique transition is a transition scenario initiated by a pair of oblique waves with equal but opposite angles. It widely exists in boundary layer flow (over flat plate, cone at zero angle of attack, two-dimensional curved plate etc.), compression ...
Ze-feng DENG, Xi CHEN, Chuan-hong ZHANG
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