Flow-field Investigation for Large-angle Cones with Short Spikes at a Mach Number of 9.6
Author : W. Frank Staylor
Publisher :
Page : 42 pages
File Size : 35,32 MB
Release : 1970
Category : Blunt bodies
ISBN :
Author : W. Frank Staylor
Publisher :
Page : 42 pages
File Size : 35,32 MB
Release : 1970
Category : Blunt bodies
ISBN :
Author :
Publisher :
Page : 1004 pages
File Size : 13,31 MB
Release : 1970
Category :
ISBN :
Author :
Publisher :
Page : 1338 pages
File Size : 38,97 MB
Release : 1970
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 1730 pages
File Size : 18,56 MB
Release : 1970
Category : Government publications
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : pages
File Size : 28,61 MB
Release : 1960-07
Category :
ISBN :
Author :
Publisher :
Page : 502 pages
File Size : 20,58 MB
Release : 2003
Category : Aeronautics
ISBN :
Author : United States. Superintendent of Documents
Publisher :
Page : 1250 pages
File Size : 47,80 MB
Release : 1979
Category : United States
ISBN :
Author :
Publisher :
Page : 974 pages
File Size : 15,81 MB
Release : 1999
Category : Aeronautics
ISBN :
Author : John David Anderson
Publisher : AIAA
Page : 710 pages
File Size : 23,90 MB
Release : 1989
Category : Science
ISBN : 9781563474590
This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.
Author : Wallace Hayes
Publisher : Elsevier
Page : 481 pages
File Size : 43,54 MB
Release : 2012-12-02
Category : Technology & Engineering
ISBN : 032314876X
Hypersonic Flow Theory presents the fundamentals of fluid mechanics, focusing on the hypersonic flow theory and approaches in theoretical aerodynamics. This book discusses the assumptions underlying hypersonic flow theory, unified supersonic-hypersonic similitude, two-dimensional and axisymmetric bodies, and circular cylinder. The constant-streamtube-area approximation, streamtube-continuity methods, and tangent-wedge and tangent-cone are also deliberated. This text likewise covers the similar laminar boundary layer solutions, bluntness induced interactions on slender bodies, and free molecule transfer theory. The dynamics of hypersonic flight or hypersonic wing theory, magnetohydrodynamic theory, or any developments involving treatment of the Boltzmann equation are not included. This publication is intended for hypersonic aerodynamicists, students, and researchers conducting work on the hypersonic flow phenomena.