Experimental Investigation of Temperature Recovery Factors on Bodies of Revolution at Supersonic Speeds

Experimental Investigation of Temperature Recovery Factors on Bodies of Revolution at Supersonic Speeds
Author: William R. Wimbrow
Publisher:
Total Pages: 26
Release: 1949
Genre: Aerodynamics, Supersonic
ISBN:
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Local temperature recovery factors have been measured on two bodies of revolution at Mach numbers of 2.0 and are shown to be independent of Mach number, Reynolds number, or body shape. The measured recovery factor is well represented by the square root of Prandtl number for laminar boundary layers and by the cube root of Prandtl number for turbulent boundary layers, as predicted by theory.


Experimental Investigation of Temperature Recovery Factors on Bodies of Revolution at Supersonic Speeds
Language: en
Pages: 26

Experimental Investigation of Temperature Recovery Factors on Bodies of Revolution at Supersonic Speeds

Authors: William R. Wimbrow
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1949 - Publisher:

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Local temperature recovery factors have been measured on two bodies of revolution at Mach numbers of 2.0 and are shown to be independent of Mach number, Reynold
An Initial Experimental Study of the Effect of Variations in Frequency and Impulse on the Reduction in Temperature Recovery Factor Afforded by Large-scale Unsteady Flow
Language: en
Pages: 28

An Initial Experimental Study of the Effect of Variations in Frequency and Impulse on the Reduction in Temperature Recovery Factor Afforded by Large-scale Unsteady Flow

Authors: Robert R. Howell
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1958 - Publisher:

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Technical Note - National Advisory Committee for Aeronautics
Language: en
Pages: 1120

Technical Note - National Advisory Committee for Aeronautics

Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1956 - Publisher:

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An Experimental Investigation of Recovery Factors and Heat-transfer Coefficients for Supersonic Air Flow Over Flat Plates
Language: en
Pages: 276

An Experimental Investigation of Recovery Factors and Heat-transfer Coefficients for Supersonic Air Flow Over Flat Plates

Authors: Robert Howard Shoulberg
Categories:
Type: BOOK - Published: 1953 - Publisher:

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Report
Language: en
Pages: 30

Report

Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1951 - Publisher:

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