An Experimental Investigation of Flat Plate Heat Transfer Coefficients at Mach Numbers of 2, 2.5, and 3 for a Surface Temperature to Stream Total Temperature Ratio of 1.18 PDF Download

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An Experimental Investigation of Flat Plate Heat Transfer Coefficients at Mach Numbers of 2, 2.5, and 3 for a Surface Temperature to Stream Total Temperature Ratio of 1.18

An Experimental Investigation of Flat Plate Heat Transfer Coefficients at Mach Numbers of 2, 2.5, and 3 for a Surface Temperature to Stream Total Temperature Ratio of 1.18 PDF Author: Robert Howard Shoulberg
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 144

Book Description

An Experimental Investigation of Flat Plate Heat Transfer Coefficients at Mach Numbers of 2, 2.5, and 3 for a Surface Temperature to Stream Total Temperature Ratio of 1.18

An Experimental Investigation of Flat Plate Heat Transfer Coefficients at Mach Numbers of 2, 2.5, and 3 for a Surface Temperature to Stream Total Temperature Ratio of 1.18 PDF Author: Robert Howard Shoulberg
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 144

Book Description

Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 934

Book Description

A Review of High-speed, Convective, Heat-transfer Computation Methods

A Review of High-speed, Convective, Heat-transfer Computation Methods PDF Author: Michael E. Tauber
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44

Book Description

Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution

Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution PDF Author: Raul J. Conti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36

Book Description

Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution

Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution PDF Author: Raul Jorge Conti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32

Book Description

Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44

Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44 PDF Author: Earl A. Price
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 46

Book Description

Experimental Convective Heat Transfer to a 4-inch and 6-inch Hemisphere at Mach Numbers from 1.62 to 3.04

Experimental Convective Heat Transfer to a 4-inch and 6-inch Hemisphere at Mach Numbers from 1.62 to 3.04 PDF Author: Leo T. Chauvin
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24

Book Description
Abstract: Equilibrium temperatures and heat-transfer coefficients for a hemispherical nose have been measured for Mach numbers from 1.62 to 3.04. Heat transfer to the surface of the hemisphere was presented as Stanton number against Reynolds number for various surface heating conditions. Heat transfer at the stagnation point has been measured and correlated with theory. Transition from a laminar to a turbulent boundary layer was obtained at Reynolds numbers of approximately 1 x 106 corresponding to a region on the body located between 45© and 60© from the stagnation point.

Journal of the Royal Aeronautical Society

Journal of the Royal Aeronautical Society PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962

Book Description

The Effect of an Arbitrary Surface-temperature Variation Along a Flat Plate on the Convective Heat Transfer in an Incompressible Turbulent Boundary Layer

The Effect of an Arbitrary Surface-temperature Variation Along a Flat Plate on the Convective Heat Transfer in an Incompressible Turbulent Boundary Layer PDF Author: Morris W. Rubesin
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 46

Book Description
An analysis was performed to determine the effects on the rates of convective heat transfer produced by arbitrary variations of the surface temperature with distance along a flat plate. The analysis was confined to the case of a low-speed turbulent boundary layer on a flat plate oriented parallel to the free-stream velocity. It was found that a continuously variable surface temperature has, in general, a smaller effect on the local convective heat transfer than does a surface-temperature discontinuity.

Journal of the Royal Aeronautical Society

Journal of the Royal Aeronautical Society PDF Author: Royal Aeronautical Society
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1164

Book Description

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