|
![]() |
|||
|
||||
OverviewThis book contains chapters written by some eminent scientists and researchers on Computational Methods in Hypersonic Aerodynamics and 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 prepared as a valuable contribution to the state-of-the-art on computational methods in hypersonic aerodynamics. All the chapters have been written by eminent scientists and researchers well known for their work in this field. Full Product DetailsAuthor: T.K.S. MurthyPublisher: Springer Imprint: Springer Edition: Softcover reprint of hardcover 1st ed. 1992 Volume: 9 Dimensions: Width: 16.00cm , Height: 2.60cm , Length: 24.00cm Weight: 0.874kg ISBN: 9789048141449ISBN 10: 9048141443 Pages: 499 Publication Date: 07 December 2010 Audience: Professional and scholarly , Professional & Vocational Format: Paperback Publisher's Status: Active Availability: Out of stock ![]() The supplier is temporarily out of stock of this item. It will be ordered for you on backorder and shipped when it becomes available. Table of ContentsReviews'In summary, this book is a useful grouping of current research papers from well-known researchers in the field of computational hypersonic aerodynamics. The book would be useful to individuals who are starting to work in this field.' AIAA Journal 31:2 1993 'In summary, this book is a useful grouping of current research papers from well-known researchers in the field of computational hypersonic aerodynamics. The book would be useful to individuals who are starting to work in this field.' AIAA Journal 31:2 1993 Author InformationTab Content 6Author Website:Countries AvailableAll regions |