Wavelet-based Adaptive Techniques Applied to Turbulent Hypersonic Scramjet Intake Flows [PDF]
The simulation of hypersonic flows is computationally demanding due to large gradients of the flow variables caused by strong shock waves and thick boundary or shear layers.
Behr, Marek+4 more
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The Development of High Order Numerical Techniques for Reentry Simulation of Hypersonic Spacecraft [PDF]
The primary difficulty encountered when simulating hypersonic flow is that the flow normally includes strong nonlinear discontinuities. These discontinuities fall into three broad classes: shocks, slip-lines, and rarefaction waves.
Sanders, Richard
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Numerical analysis of a hypersonic turbulent and laminar flow using a commercial cfd solver [PDF]
Computational fluid dynamics computations for two hypersonic flow cases using the commercial ANSYS FLUENT 16.2 CFD software were done. In this paper, an internal and external hypersonic flow cases were considered and analysis of the hypersonic flow using
Ivanov, Toni+4 more
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Hypersonic aerodynamic problems at re-entry of space vehicles [PDF]
Hypersonic aerodynamic problems at space vehicle reentry - plasma effects on communications blackout, hypersonic flow, and atmospheric ...
Hermann, R.
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Experimental investigation of hypersonic buzz on a high cross-range shuttle configuration [PDF]
A wind tunnel investigation has been conducted to determine the nature of an unsteady hypersonic flow phenomenon, often referred to as hypersonic buzz, on a 1:100 scale model representative of a high cross-range shuttle configuration.
Goldman, R. L., Obremski, H. J.
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Computational analysis of hypersonic airbreathing aircraft flow fields [PDF]
The general problem of calculating the flow fields associated with hypersonic airbreathing aircraft is presented. Unique aspects of hypersonic aircraft aerodynamics are introduced and their demands on computational fluid dynamics are outlined.
Dwoyer, Douglas L., Kumar, Ajay
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Numerical simulation of the hypersonic flow around lifting vehicles [PDF]
A method for solving the viscous hypersonic flow field around realistic configurations is presented. The numerical procedure for generating the required finite difference grid and the two-factored implicit flow solver are described. Results are presented
Chaussee, Denny+2 more
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Hypersonic turbulent wall boundary layer computations [PDF]
The Baldwin-Lomax algebraic turbulence model was modified for hypersonic flow conditions. Two coefficients in the outer layer eddy viscosity model were determined as functions of Mach number and temperature ratio.
Harloff, G. J., Kim, S. C.
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Transition to turbulence in laminar hypersonic flow [PDF]
Progress in a recently started project aimed at the prediction of transition to turbulence in hypersonic flow is briefly discussed. The prediction of transition to turbulence is a very important issue in the design of space vessels.
Vandervegt, Jaap
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Laminar flow past a sphere at high mach number [PDF]
Hypersonic viscous flow past ...
Chyu, W. J., Davis, R. T.
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