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Date : 1990-02-01
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Nonequilibrium Hypersonic Aerothermodynamics Chul Park ~ Presents the principles of aerothermodynamics in nonequilibrium hypersonic flow regimes covering theory application and surface phenomena Chapters 1 to 5 explain how to develop computational fluid dynamics CFD techniques for computing nonequilibrium chemically reacting flows in the hypersonic regime
Nonequilibrium Hypersonic Aerothermodynamics by Chul Park ~ Nonequilibrium Hypersonic Aerothermodynamics Describes the interaction between the fluid flow and the high temperature phenomena experienced in the hypersonic regime Presents the principles of aerothermodynamics in nonequilibrium hypersonic flow regimes covering theory application and surface phenomena
Nonequilibrium Hypersonic Aerothermodynamics By C PARK ~ Nonequilibrium Hypersonic Aerothermodynamics By C PARK Wiley 1990 358 pp £4750 Volume 233 R A East Skip to main content Accessibility help We use cookies to distinguish you from other users and to provide you with a better experience on our websites
PDF Nonequilibrium Hypersonic Aerothermodynamics Using ~ Abstract Hypersonic flight vehicles are a current topic of interest in both civilian and military research NASA is currently designing a Crew Transport Vehicle CTV 44 69 and Crew Exploration Vehicle CEV 32 to replace the space shuttle reentry vehicles are by definition hypersonic vehicles
Nonequilibrium Hypersonic Aerothermodynamics Physics ~ This option allows users to search by Publication Volume and Page Selecting this option will search the current publication in context Selecting this option will search all publications across the Scitation platform Selecting this option will search all publications for the PublisherSociety in context
NONEQUILIBRIUM HYPERSONIC AEROTHERMODYNAMICS USING THE ~ NONEQUILIBRIUM HYPERSONIC AEROTHERMODYNAMICS USING THE DIRECT SIMULATION MONTE CARLO AND NAVIERSTOKES MODELS by Andrew J Lofthouse A dissertation submitted in partial fulflllment of the requirements for the degree of Doctor of Philosophy Aerospace Engineering in The University of Michigan 2008 Doctoral Committee Professor Iain D Boyd Chair
Hypersonic Aerothermodynamics Southwest Research Institute ~ Hypersonic Aerothermodynamics At hypersonic speeds modeling vehicle aerodynamic performance surface heating and wake dynamics requires complex multiphysics and multiscale simulations Aerodynamic drag and heating are strongly affected by the chemical and thermal nonequilibrium environments surface chemistry ablation shockboundary layer interactions and boundary layer transition effects
Hypersonic Nonequilibrium Flows Fundamentals and Recent ~ Hypersonic Nonequilibrium Flows includes fundamental governing equations of nonequilibrium fluid transport and computational approach to calculation of rates and crosssections in quantized energy states DSMC approach radiative heat transfer a CFD perspective surface chemistry with additional chapters on high enthalpy facilities and the associated diagnostic techniques
Nonequilibrium Aerothermodynamics for a Capsule Reentry ~ Real gas aerothermodynamics and catalytic effects on the vehicle forebody heat shield have been taken into account To this end several NavierStokes computational fluid dynamics analyses have been performed in correspondence with the reentry peak heating conditions by considering the air as a nonequilibrium reacting gas mixture
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