Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations. Volume 2: Code description [PDF]
A numerical procedure was developed to compute the inviscid super/hypersonic flow field about complex vehicle geometries accurately and efficiently.
Marconi, F., Yaeger, L.
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Numerical investigation of compressible flow around nose cone with Multi-row disk and multi coolant jets. [PDF]
Iranmanesh R+3 more
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Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations. Volume 1: Computational technique [PDF]
A numerical procedure has been developed to compute the inviscid super/hypersonic flow field about complex vehicle geometries accurately and efficiently.
Marconi, F., Salas, M., Yaeger, L.
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Zirconium Carbide for Hypersonic Applications, Opportunities and Challenges. [PDF]
Peterson GR, Carr RE, Marinero EE.
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Numerical computation of space shuttle orbiter flow field [PDF]
A new parabolized Navier-Stokes (PNS) code has been developed to compute the hypersonic, viscous chemically reacting flow fields around 3-D bodies. The flow medium is assumed to be a multicomponent mixture of thermally perfect but calorically imperfect ...
Tannehill, John C.
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A Quick Simulation Method for Aero-Optical Effects Based on a Density Proxy Model. [PDF]
Yang B+5 more
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Computational analysis of hypersonic flows past elliptic-cone waveriders [PDF]
A comprehensive study for the inviscid numerical calculation of the hypersonic flow past a class of elliptic-cone derived waveriders is presented. The theoretical background associated with hypersonic small-disturbance theory (HSDT) is reviewed.
Rasmussen, Maurice L., Yoon, Bok-Hyun
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High speed corner and gap-seal computations using an LU-SGS scheme [PDF]
The hybrid Lower-Upper Symmetric Gauss-Seidel (LU-SGS) algorithm was added to a widely used series of 2D/3D Euler/Navier-Stokes solvers and was demonstrated for a particular class of high-speed flows.
Coirier, William J.
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Magnetohydrodynamic simulations of hypersonic flow over a cylinder using axial- and transverse-oriented magnetic dipoles. [PDF]
Guarendi AN, Chandy AJ.
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Experimental research of the aerodynamics of nozzles and plumes at hypersonic speeds [PDF]
The purpose was to experimentally characterize the flow field created by the interaction of a single expansion ramp nozzle (SERN) flow with a hypersonic external stream.
Keener, Earl R.
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