Transonic Aerodynamic Characteristics of a Medium Hypersonic LD Reentry Spacecraft with a Variable Geometry Wing
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Page : 100 pages
File Size : 21,27 MB
Release : 1970
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Page : 100 pages
File Size : 21,27 MB
Release : 1970
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Page : 356 pages
File Size : 41,57 MB
Release : 1970
Category : Aeronautics
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Page : 1166 pages
File Size : 15,96 MB
Release : 1970
Category : Aeronautics
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Page : 710 pages
File Size : 39,95 MB
Release : 1970
Category : Science
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Page : 1228 pages
File Size : 30,44 MB
Release : 1970
Category : Technology
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Page : 1416 pages
File Size : 44,10 MB
Release : 1970
Category : Science
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Page : 970 pages
File Size : 38,97 MB
Release : 1970
Category : Science
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Page : 940 pages
File Size : 34,71 MB
Release : 1970-07
Category : Science
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Author : United States. National Aeronautics and Space Administration
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Page : 792 pages
File Size : 32,48 MB
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Author : John David Anderson
Publisher : AIAA
Page : 710 pages
File Size : 31,26 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.