Pressure Distribution on a Blunt-leading-edge Modified-delta-planform Reentry Configuration at a Mach Number of 6.0
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Page : 32 pages
File Size : 41,58 MB
Release : 1963
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Page : 32 pages
File Size : 41,58 MB
Release : 1963
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Page : 1274 pages
File Size : 34,4 MB
Release : 1961
Category : Government publications
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Author : United States. Superintendent of Documents
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Page : 1284 pages
File Size : 15,79 MB
Release : 1980
Category : United States
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Author : United States. Superintendent of Documents
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Page : 1284 pages
File Size : 42,2 MB
Release : 1961
Category : Government publications
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Page : 1572 pages
File Size : 15,19 MB
Release : 1969
Category : Aeronautics
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Page : 962 pages
File Size : 43,86 MB
Release : 1962
Category : Aeronautics
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Author : Royal Aeronautical Society
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Page : 1164 pages
File Size : 36,31 MB
Release : 1962
Category : Aeronautics
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Page : 526 pages
File Size : 27,13 MB
Release : 1997
Category : Aeronautics
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Page : 1060 pages
File Size : 38,15 MB
Release : 1997
Category : Mechanics, Applied
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Author : John David Anderson
Publisher : AIAA
Page : 710 pages
File Size : 29,94 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.