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Author : Robert Wesley Truitt
Publisher : Unknown
Page : 486 pages
File Size : 41,7 Mb
Release : 1980
Category : Aerodynamics, Hypersonic
ISBN : OSU:32435012497152
Author : James R. Batt,Richard H. Gallagher,Rolland D. Huff,James F. Quinn,Joseph Padlog,Vincent W. Donato
Publisher : Unknown
Page : 392 pages
File Size : 49,5 Mb
Release : 1963
Category : Aerodynamics, Hypersonic
ISBN : UOM:39015095319292
Author : V.Z. Parton
Publisher : Routledge
Page : 209 pages
File Size : 41,5 Mb
Release : 2018-03-29
Category : Technology & Engineering
ISBN : 9781351412933
Recent government and commercial efforts to develop orbital and suborbital passenger and transport aircraft have resulted in a burgeoning of new research. The articles in this book, translated from Russian, were contributed by the world's leading authorities on supersonic and hypersonic flows and heat transfer. This superb book addresses the physics and engineering aspects of ultra high-speed aerodynamic problems. Thorough coverage is given to an array of specific problem-solving equations. Super- and Hypersonic Aerodynamics and Heat Transfer will be essential reading for all aeronautical engineers, mechanical engineers, mathematicians, and physicists involved in this exciting field of research.
Author : John David Anderson
Publisher : AIAA
Page : 710 pages
File Size : 43,9 Mb
Release : 1989
Category : Science
ISBN : 156347459X
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 : G. G. Chernyi
Publisher : Academic Press
Page : 276 pages
File Size : 46,7 Mb
Release : 2013-10-22
Category : Technology & Engineering
ISBN : 9781483271682
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 : Robert M. Bennett
Publisher : Unknown
Page : 68 pages
File Size : 50,8 Mb
Release : 1972
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112106882845
The method of integral relations is applied in a one-strip approximation to the perturbation equations governing small motions of an inclined, sharp-edged, flat surface about the mean supersonic steady flow. Algebraic expressions for low reduced-frequency aerodynamics are obtained and a set of ordinary differential equations are obtained for general oscillatory motion. Results are presented for low reduced-frequency aerodynamics and for the variation of the unsteady forces with frequency. The method gives accurate results for the aerodynamic forces at low reduced frequency which are in good agreement with available experimental data. However, for cases in which the aerodynamic forces vary rapidly with frequency, the results are qualitatively correct, but of limited accuracy. Calculations indicate that for a range of inclination angles near shock detachment such that the flow in the shock layer is low supersonic, the aerodynamic forces vary rapidly both with inclination angle and with reduced frequency.
Author : D. Adamson,E. A. Bonney,I. D. V. Faro
Publisher : Unknown
Page : 366 pages
File Size : 42,7 Mb
Release : 1961
Category : Aerodynamics, Supersonic
ISBN : UOM:39015104955268
Author : Johns Hopkins University. Applied Physics Laboratory,Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md
Publisher : Unknown
Page : 364 pages
File Size : 41,8 Mb
Release : 1966
Category : Aerodynamics, Supersonic
ISBN : OSU:32435023080864
Author : I. I. Glass,J. Gordon Hall
Publisher : Unknown
Page : 642 pages
File Size : 51,8 Mb
Release : 1959
Category : Aerodynamics, Supersonic
ISBN : UOM:39015104975050
Author : Giuseppe Pezzella,Antonio Viviani
Publisher : BoD – Books on Demand
Page : 150 pages
File Size : 51,6 Mb
Release : 2019-10-02
Category : Science
ISBN : 9781839622694
In the aviation field there is great interest in high-speed vehicle design. Hypersonic vehicles represent the next frontier of passenger transportation to and from space. However, several design issues must be addressed, including vehicle aerodynamics and aerothermodynamics, aeroshape design optimization, aerodynamic heating, boundary layer transition, and so on. This book contains valuable contributions focusing on hypervelocity aircraft design. Topics covered include hypersonic aircraft aerodynamic and aerothermodynamic design, especially aeroshape design optimization, computational fluid dynamics, and scramjet propulsion. The book also discusses high-speed flow issues and the challenges to achieving the dream of affordable hypersonic travel. It is hoped that the information contained herein will allow for the development of safe and efficient hypersonic vehicles.
Author : John J. Bertin
Publisher : AIAA
Page : 644 pages
File Size : 49,9 Mb
Release : 1994
Category : Science
ISBN : 1563470365
A modern treatment of hypersonic aerothermodynamics for students, engineers, scientists, and program managers involved in the study and application of hypersonic flight. It assumes an understanding of the basic principles of fluid mechanics, thermodynamics, compressible flow, and heat transfer. Ten chapters address: general characterization of hypersonic flows; basic equations of motion; defining the aerothermodynamic environment; experimental measurements of hypersonic flows; stagnation-region flowfield; the pressure distribution; the boundary layer and convective heat transfer; aerodynamic forces and moments; viscous interactions; and aerothermodynamics and design considerations. Includes sample exercises and homework problems. Annotation copyright by Book News, Inc., Portland, OR
Author : R. E. Wilson
Publisher : Unknown
Page : 364 pages
File Size : 41,7 Mb
Release : 1966
Category : Heat
ISBN : UOM:39015104956050
Author : George Rudinger
Publisher : Unknown
Page : 452 pages
File Size : 52,5 Mb
Release : 1964
Category : Aerodynamics, Supersonic
ISBN : UOM:39015104975068
Author : J. J. Chattot,M. M. Hafez
Publisher : Springer
Page : 620 pages
File Size : 50,5 Mb
Release : 2015-03-31
Category : Science
ISBN : 9789401798259
This book covers classical and modern aerodynamics, theories and related numerical methods, for senior and first-year graduate engineering students, including: -The classical potential (incompressible) flow theories for low speed aerodynamics of thin airfoils and high and low aspect ratio wings. - The linearized theories for compressible subsonic and supersonic aerodynamics. - The nonlinear transonic small disturbance potential flow theory, including supercritical wing sections, the extended transonic area rule with lift effect, transonic lifting line and swept or oblique wings to minimize wave drag. Unsteady flow is also briefly discussed. Numerical simulations based on relaxation mixed-finite difference methods are presented and explained. - Boundary layer theory for all Mach number regimes and viscous/inviscid interaction procedures used in practical aerodynamics calculations. There are also four chapters covering special topics, including wind turbines and propellers, airplane design, flow analogies and hypersonic (rotational) flows. A unique feature of the book is its ten self-tests and their solutions as well as an appendix on special techniques of functions of complex variables, method of characteristics and conservation laws and shock waves. The book is the culmination of two courses taught every year by the two authors for the last two decades to seniors and first-year graduate students of aerospace engineering at UC Davis.
Author : Robert W. Truitt
Publisher : Unknown
Page : 462 pages
File Size : 52,5 Mb
Release : 1959-05-01
Category : Electronic
ISBN : 0471066931