The Investigation for the Aerodynamic and Heat Transfer Characteristics of Slender Hypersonic Cones Over a Wide Range of Angles of Attack PDF Download
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Author: Paul K. Chang
Publisher:
ISBN:
Category :
Languages : en
Pages : 133
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Book Description
The problems of aerodynamic and heat transfer characteristics of slender sharp nosed hypersonic cones over a wide range of angles of attack are examined and the analytical solutions are presented. Three particular problems are studied: (1) inviscid flow characteristics of shock layer involving laminar separation in the leeward side with undisturbed free stream Mach number 7.95 and angle of attack 20 degrees for cone half angle 10 degrees, (2) attached three-dimensional compressible boundary layer over the cone, (3) aerodynamic and heat transfer characteristics of turbulent separated flow. (Author).
Author: Paul K. Chang
Publisher:
ISBN:
Category :
Languages : en
Pages : 133
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Book Description
The problems of aerodynamic and heat transfer characteristics of slender sharp nosed hypersonic cones over a wide range of angles of attack are examined and the analytical solutions are presented. Three particular problems are studied: (1) inviscid flow characteristics of shock layer involving laminar separation in the leeward side with undisturbed free stream Mach number 7.95 and angle of attack 20 degrees for cone half angle 10 degrees, (2) attached three-dimensional compressible boundary layer over the cone, (3) aerodynamic and heat transfer characteristics of turbulent separated flow. (Author).
Author: Robert H. Feldhuhn
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 148
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Book Description
Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 2/3 power law body and two ducted-cone configurations.
Author: Robert H. Feldhuhn
Publisher:
ISBN:
Category :
Languages : en
Pages : 119
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Book Description
Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 2/3 power law body and two ducted-cone configurations.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1134
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Book Description
Author: Joseph W. Cleary
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 52
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Book Description
Author: V. S. Nikolaev
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 20
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Book Description
Author:
Publisher:
ISBN:
Category : Nuclear energy
Languages : en
Pages : 78
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Book Description
Author: Donald M. Wilson
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 94
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Book Description
Turbulent boundary layer heat transfer rates were measured on a thin-walled slender cone at a free-stream Mach number of 5.0. Wall to stagnation temperature ratios from 0.15 to 0.40 were obtained by pre-cooling the model using liquid nitrogen. Tests at a wide range of Reynolds numbers were conducted by varying the tunnel supply pressure; thus providing data for both laminar and mixed laminar-turbulent types of boundary layers. The experimental results obtained were compared with existing theories which predict convective heat transfer coefficients. These comparisons indicate that the data corresponding to a 760R supply temperature verify the predictions of Winkler and Cha; however, data acquired at a supply temperature of 1160R substantiate the predictions of Spalding and Chi. (Author).
Author: V.Z. Parton
Publisher: Routledge
ISBN: 1351412930
Category : Technology & Engineering
Languages : en
Pages : 209
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Book Description
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: Michael E. Tauber
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
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Book Description
