Super And Hypersonic Aerodynamics And Heat Transfer

Author : V.Z. Parton
Publisher : Routledge
Page : 209 pages
File Size : 45,7 Mb
Release : 2018-03-29
Category : Technology & Engineering
ISBN : 9781351412933

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Super- and Hypersonic Aerodynamics and Heat Transfer by V.Z. Parton Pdf

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 J. Bertin
Publisher : AIAA
Page : 644 pages
File Size : 45,8 Mb
Release : 1994
Category : Science
ISBN : 1563470365

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Hypersonic Aerothermodynamics by John J. Bertin Pdf

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 : Sergey V. Utyuzhnikov,Grigoriĭ Aleksandrovich Tirskiĭ
Publisher : Begell House Publishers
Page : 536 pages
File Size : 42,6 Mb
Release : 2014-01
Category : Aerodynamics, Hypersonic
ISBN : 1567003095

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Hypersonic Aerodynamics and Heat Transfer by Sergey V. Utyuzhnikov,Grigoriĭ Aleksandrovich Tirskiĭ Pdf

Author : Anonim
Publisher : Unknown
Page : 0 pages
File Size : 45,9 Mb
Release : 2014
Category : Aerodynamics, Hypersonic
ISBN : 1567002870

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Hypersonic Aerodynamics and Heat Transfer by Anonim Pdf

The book presents recent theoretical and experimental results achieved in Russia in the field of aerothermodynamics of hypersonic flows over complex configurations. These results include analysis of gas flows over the space shuttle 'Buran', various aircraft configurations and interplanetary vehicles.

Author : John David Anderson
Publisher : AIAA
Page : 710 pages
File Size : 40,6 Mb
Release : 1989
Category : Science
ISBN : 156347459X

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Hypersonic and High Temperature Gas Dynamics by John David Anderson Pdf

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 : Richard Scherrer
Publisher : Unknown
Page : 540 pages
File Size : 46,6 Mb
Release : 1947
Category : Aerodynamic heating
ISBN : STANFORD:36105024795457

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The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight by Richard Scherrer Pdf

An approximate method for determining the convective cooling requirement in the laminar-boundary-layer region of a body of revolution in high-speed flight was developed and applied to an example body. The cooling requirement for the example body was determined as a function of Mach number, altitude, size, and a surface-temperature parameter. The maximum value of Mach number considered was 3.0 and the altitudes considered were those within the lower constant-temperature region of the atmosphere (40,000 to 120,000 ft). The extent of the laminar boundary layer was determined approximately at each condition as a function of the variables considered.

Author : Wilbur C. Nelson
Publisher : Elsevier
Page : 800 pages
File Size : 55,6 Mb
Release : 2014-12-02
Category : Science
ISBN : 9781483223315

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The High Temperature Aspects of Hypersonic Flow by Wilbur C. Nelson Pdf

The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.

Author : Victor Zakkay
Publisher : Unknown
Page : 66 pages
File Size : 41,5 Mb
Release : 1958
Category : Aerodynamics, Hypersonic
ISBN : UOM:39015095330257

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Pressure and Laminar Heat Transfer Results in Three-dimensional Hypersonic Flow by Victor Zakkay Pdf

Author : Antonio Ferri
Publisher : Unknown
Page : 72 pages
File Size : 42,9 Mb
Release : 1959
Category : Aerodynamics, Hypersonic
ISBN : UOM:39015104979920

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Some Heat Transfer Problems in Hypersonic Flow by Antonio Ferri Pdf

Author : Hung-Ta Ho,Ronald F. Probstein
Publisher : Unknown
Page : 90 pages
File Size : 49,7 Mb
Release : 1958
Category : Aerodynamics, Hypersonic
ISBN : UOM:39015104979433

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A Series Solution to the Laminar Heat Transfer Problem at Hypersonic Speeds by Hung-Ta Ho,Ronald F. Probstein Pdf

Author : Louis G. Kaufman
Publisher : Unknown
Page : 172 pages
File Size : 44,8 Mb
Release : 1964
Category : Aerodynamic heating
ISBN : UOM:39015095304153

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Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 8 heat transfer data for flows ahead of ramps by Louis G. Kaufman Pdf

"Pressure and heat transfer data were obtained for hypersonic flows over 40-degree expansion corners and ahead of ramps. Full and partial span ramps, having wedge angles up to 90 degrees, were tested at two locations on a sharp leading edge flat plate, with and without end plates. Pressure data were obtained for [M sub infinity =] 5 for model length Reynolds numbers between 1.1 and 6.6 million. Both pressure and heat transfer data were obtained for [M sub infinity =] 8 for Reynolds numbers between 1.1 and 3.3 million." -- page iii, pt.4.

Author : Anonim
Publisher : Unknown
Page : 100 pages
File Size : 41,9 Mb
Release : 1960
Category : Aerodynamics, Hypersonic
ISBN : UOM:39015095265644

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Hypersonic Free Flight Research: Investigations of heat trasfer and aerodynamic stability, by O. R. Burggraf by Anonim Pdf

Author : Anonim
Publisher : Springer Nature
Page : 554 pages
File Size : 52,6 Mb
Release : 1989
Category : Electronic
ISBN : 9781468491876

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Hypersonics by Anonim Pdf

Author : Mostafa Barzegar Gerdroodbary
Publisher : Elsevier
Page : 248 pages
File Size : 44,7 Mb
Release : 2022-10-11
Category : Technology & Engineering
ISBN : 9780323972239

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Aerodynamic Heating in Supersonic and Hypersonic Flows by Mostafa Barzegar Gerdroodbary Pdf

Aerodynamic Heating in Supersonic and Hypersonic Flows: Advanced Techniques for Drag and Aero-heating Reduction explores the pros and cons of different heat reduction techniques on other characteristics of hypersonic vehicles. The book begins with an introduction of flow feature around the forebody of space vehicles and explains the main parameters on drag force and heat production in this region. The text then discusses the impact of severe heat production on the nose of hypervelocity vehicles, different reduction techniques for aerodynamic heating, and current practical applications for forebody shock control devices. Delivers valuable insight for aerospace engineers, postgraduate students, and researchers. Presents computational results of different cooling systems for drag and heat reduction around nose cones Explains mechanisms of drag reduction via mechanical, fluidic, and thermal systems Provides comprehensive details about the aerodynamics of space vehicles and the different shock features in the forebody of super/hypersonic vehicles Describes how numerical simulations are used for the development of the current design of forebody of super/hypersonic vehicles

Author : Ramesh K. Agarwal
Publisher : BoD – Books on Demand
Page : 186 pages
File Size : 45,7 Mb
Release : 2018-03-14
Category : Technology & Engineering
ISBN : 9789535139034

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Advances in Some Hypersonic Vehicles Technologies by Ramesh K. Agarwal Pdf

The book describes the recent progress in some hypersonic technologies such as the aerodynamic modeling and numerical simulations of rarefied flows, boundary layer receptivity, coupled aerodynamics, and heat transfer problems, including fluid-thermal-structure interactions and launcher aerodynamic design as well as other miscellaneous topics, such as porous ceramic composite phase change control system and vehicle profile, following LQR design. Both the researchers and the students should find the material useful in their work.