Viscous shock layer solutions for turbulent flow of radiating gas mixtures in chemical equilibrium [PDF]
The viscous shock layer equations for hypersonic laminar and turbulent flows of radiating or nonradiating gas mixtures in chemical equilibrium are presented for two-dimensional and axially symmetric flow fields.
Anderson, E. C., Moss, J. N.
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Research on the drag reduction performance induced by the counterflowing jet for waverider with variable blunt radii [PDF]
, 2016 Waverider will endure the huge aero-heating in the hypersonic flow, thus, it need be blunt for the leading edge. However, the aerodynamic performance will decrease for the blunt waverider because of the drag hoik.
Barakos, George N. +4 more
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Hypersonic laminar boundary layers around slender bodies [PDF]
Compressible laminar boundary layer equations considered for hypersonic flow around slender ...
Jeng, D. R., Yalamanchili, R. V. S.
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Studies related to the design of a magnetic suspension and balance system Interim technical report, Dec. 1964 - Jan. 1966 [PDF]
Magnetic suspension and balance system for use in hypersonic flow ...
Basmajian, V. V. +2 more
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Hypersonic aerodynamics on thin bodies with interaction and upstream influence [PDF]
, 1994 In the fundamental configuration studied here, a steady hypersonic free stream flows over a thin sharp aligned airfoil or flat plate with a leading-edge shock wave, and the flow field in the shock layer (containing a viscous and an inviscid layer) is ...
Khorrami, AF, Smith, FT
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Multigrid for hypersonic inviscid flows [PDF]
The use of multigrid methods to solve the Euler equations for hypersonic flow is discussed. The steady state equations are considered with a Runge-Kutta smoother based on the time accurate equations together with local time stepping and residual ...
Decker, Naomi H., Turkel, Eli
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Analysis of thermochemical non-equilibrium hypersonic flow over a waverider with uncertainty quantification [PDF]
arXivThe objective of this work is to assess the impact of parameter uncertainty on hypersonic aerothermal surface heating predictions in Reynolds-Averaged Navier-Stokes (RANS) simulations using non-intrusive uncertainty quantification (UQ) techniques. RANS-based models are considered indispensable tools in computational fluid dynamics (CFD) analysis for ...
arxiv
Hypersonic blunt-body flow of a radiating gas at low density [PDF]
Hypersonic blunt body flow of radiating gas at low ...
Schneider, W. A.
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General Reynolds Analogy for Blunt-nosed Bodies in Hypersonic Flows [PDF]
arXiv, 2015 In this paper, the relation between skin friction and heat transfer along windward sides of blunt-nosed bodies in hypersonic flows is investigated. The self-similar boundary layer analysis is accepted to figure out the distribution of the ratio of skin friction to heat transfer coefficients along the wall.
arxiv
Experiments with Magnetohydrodynamically Supported Shock Layers [PDF]
Shock tube experiments to determine interaction of hypersonic flow with magnetic ...
Locke, E., Petschek, H. E., Rose, P. H.
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