Del i serien Fluid Mechanics and Its Applications

Computational Methods in Hypersonic Aerodynamics

Inbunden, Engelska, 1992

AvT.K.S. Murthy

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Written by some scientists and researchers on Computational Methods in Hypersonic Aerodynamics, this work forms a natural sequel to the earlier publications on Computational Methods in Potential Flow (1986) and Computational Methods in Viscous Aerodynamics (1990). In this book, the earlier attempts at the solution of the highly nonlinear Navier-Stokes equations are extended to the aerothermodynamics of flow in the hypersonic regime, including the effects of viscosity on the physical and chemical processes of high-temperature nonequilibrium flow at very high speeds, such as vibrational excitation, dissociation and recombination, ionization and radiation, as well as real gas effects and the effects of high temperature and low density. The book has been designed to make a valuable contribution to the state-of-the-art on computational methods in hypersonic aerodynamcis.

Produktinformation

Utgivningsdatum1992-03-31
Mått155 x 235 x 33 mm
Vikt934 g
FormatInbunden
SpråkEngelska
SerieFluid Mechanics and Its Applications
Antal sidor499
Upplaga1992
FörlagKluwer Academic Publishers
ISBN9780792316732

Tillhör följande kategorier

Introduction to the physical aspects of hypersonic aerodynamics, R. Grundmann; Computational methods for viscous hypersonic flow, D. Hanel; Numerical simulation of hypersonic flows, J.S. Shang; Point-implicit relaxation strategies for viscous hypersonic flows, P.A. Gnoffo; Flux-split algorithms for hypersonic flows, P. Cinnella, B. Grossman; Efficient multigrid computation of steady hypesonic flows, B. Koren, P.W. Hemker; Laminar turbulent transition, D. Arnal; Second-order effects in hypersonic laminar boundary layers, J.Ph. Brazier et al; Real gas effects in two and three-dimensional hypersonic, laminar boundary layers, B. Aupoix, J. Cousteix; Flow analysis and design optimization methods for nozzle-afterbody of a hypersonic vehicle, O. Baysal; The computation over unstructured grids of inviscid hypersonic reactive flow by upwind finite-volume schemes, J.A. Desideri; Computational aerothermodynamics for 2D and 3D space vehicles, J. Hauser et al.