Super- and Hypersonic Aerodynamics and Heat Transfer

Super- and Hypersonic Aerodynamics and Heat Transfer PDF

Author: V.Z. Parton

Publisher: Routledge

Published: 2018-03-29

Total Pages: 209

ISBN-13: 1351412930

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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.

Super- and Hypersonic Aerodynamics and Heat Transfer

Super- and Hypersonic Aerodynamics and Heat Transfer PDF

Author: V.Z. Parton

Publisher: Routledge

Published: 2018-03-29

Total Pages: 352

ISBN-13: 1351412949

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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.

Hypersonic Aerothermodynamics

Hypersonic Aerothermodynamics PDF

Author: John J. Bertin

Publisher: AIAA

Published: 1994

Total Pages: 644

ISBN-13: 9781563470363

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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

Hypersonic Aerodynamics and Heat Transfer

Hypersonic Aerodynamics and Heat Transfer PDF

Author: Sergey Vladimirovich Utjužnikov

Publisher:

Published: 2013

Total Pages: 383

ISBN-13: 9781567002874

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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.

Hypersonic Aerodynamics and Heat Transfer

Hypersonic Aerodynamics and Heat Transfer PDF

Author:

Publisher:

Published: 2014

Total Pages: 0

ISBN-13: 9781567002874

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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.

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

The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight PDF

Author: Richard Scherrer

Publisher:

Published: 1947

Total Pages: 542

ISBN-13:

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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.

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

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 PDF

Author: Louis G. Kaufman

Publisher:

Published: 1964

Total Pages: 172

ISBN-13:

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"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.

Aerodynamic Heating in Supersonic and Hypersonic Flows

Aerodynamic Heating in Supersonic and Hypersonic Flows PDF

Author: Mostafa Barzegar Gerdroodbary

Publisher: Elsevier

Published: 2022-10-11

Total Pages: 248

ISBN-13: 0323972233

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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

Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 8 pressure data for flows ahead of ramps

Pressure and Heat Transfer Measurements for Hypersonic Flows Over Expansion Corners and Ahead of Ramps: Mach 8 pressure data for flows ahead of ramps PDF

Author: Louis G. Kaufman

Publisher:

Published: 1964

Total Pages: 144

ISBN-13:

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"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.

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