The Hypersonic Leading Edge Problem Ii Wedges And Cones
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Author | : |
Publisher | : |
Total Pages | : 758 |
Release | : 1979 |
Genre | : Aeronautics |
ISBN | : |
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author | : |
Publisher | : |
Total Pages | : 840 |
Release | : 1989 |
Genre | : Astronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 44 |
Release | : 1989 |
Genre | : Aeronautics |
ISBN | : |
Author | : David E. Boylan |
Publisher | : |
Total Pages | : 68 |
Release | : 1973 |
Genre | : Aerodynamic heating |
ISBN | : |
The report presents heat-transfer-rate measurements on sharp and blunt 10-deg half-angle cones at angles of attack between -9 and +10 deg in a low-density, hypersonic wind tunnel. Circumferential and longitudinal distributions are presented for cold wall conditions for a range at Mach and Reynolds numbers. The effect of source-like flows was studied by utilizing both conical and contoured expansion nozzles with the same free-stream similarity parameters and model wall temperatures. Comparisons are made with previously published experimental and theoretical results. (Author).
Author | : Michael E. Tauber |
Publisher | : |
Total Pages | : 44 |
Release | : 1989 |
Genre | : Aerodynamic heating |
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Author | : |
Publisher | : |
Total Pages | : 628 |
Release | : 1974 |
Genre | : Mechanics, Applied |
ISBN | : |
Author | : G. G. Chernyi |
Publisher | : Academic Press |
Total Pages | : 277 |
Release | : 2013-10-22 |
Genre | : Technology & Engineering |
ISBN | : 1483271684 |
Introduction to Hypersonic Flow has been made available to the English speaking reader because of its usefulness for those individuals desirous of obtaining an introduction to the subject. Written by an internationally acknowledged expert in the field of hypersonic flow, the book makes available heretofore unpublished Soviet work, as well as published work little known outside the Soviet Union. The author has however made every effort to include, where appropriate. Western references for the work he discusses. Starting with a general introductory chapter on hypersonic aerodynamics and aerodynamic problems, the remainder of the book concentrates on the inviscid, perfect fluid aspects of hypersonic flow, with emphasis on the fundamental concepts and rational methods of calculation. The book is directed to students of aerodynamics and gas dynamics, as well as to scientists and engineers interested in problems of hypersonic flight. The level of approach is such that it should prove particularly useful as an undergraduate and introductory graduate text.
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 796 |
Release | : 1962 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 1526 |
Release | : 1974 |
Genre | : Electronic journals |
ISBN | : |
Author | : John David Anderson |
Publisher | : AIAA |
Total Pages | : 710 |
Release | : 1989 |
Genre | : 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.