The Flow Field Over Blunted Flat Plates and Its Effect on Turbulent Boundary-layer Growth and Heat Transfer at a Mach Number of 4.7 PDF Download
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Author: Thorval Tendeland
Publisher:
ISBN:
Category :
Languages : en
Pages : 59
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Book Description
Author: Thorval Tendeland
Publisher:
ISBN:
Category :
Languages : en
Pages : 59
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Book Description
Author: Thorval Tendeland
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64
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Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Military art and science
Languages : en
Pages : 1746
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Author: Neal Tetervin
Publisher:
ISBN:
Category : Skin friction (Aerodynamics)
Languages : en
Pages : 168
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Book Description
The concepts of eddy kinematic viscosity and eddy diffusivity are used to calculate skin friction and heat transfer coefficients for the turbulent boundary layer on a flat plate. The eddy kinematic viscosity, eddy diffusivity, and turbulent Prandtl number vary across the boundary layer. The Mach number range is from zero to ten. The surface to stream temperature ratio varies from one-half to eight, and includes the insulated surface. The friction results are compared with experimental data. Velocity and temperature profiles for the entire region from the surface to the outer edge are compared with experimental data. (Author).
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 986
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 508
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Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 654
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 852
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1878
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Author: Ernst Rudolf Georg Eckert
Publisher: Elsevier Science & Technology
ISBN:
Category : Science
Languages : en
Pages : 576
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