An Extension of the Investigation of the Effects of Heat Transfer on Boundary-layer Transition on a Parabolic Body of Revolution (NACA RM-10) at a Mach Number of 1.61

An Extension of the Investigation of the Effects of Heat Transfer on Boundary-layer Transition on a Parabolic Body of Revolution (NACA RM-10) at a Mach Number of 1.61
Author: K. R. Czarnecki
Publisher:
Total Pages: 21
Release: 1954
Genre: Body of revolution
ISBN:

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The results indicate that the trend found previously of an increase in boundary-layer transition Reynolds number with increase in model cooling continued to higher Reynolds numbers. The highest transition Reynolds number obtained with cooling was 28,500,000. At this Reynolds number, the classical Tollmien-Schlichting wave type of boundary-layer number, the instability was apparently overshadowed by surface roughness effects. The results indicated that, when transition was fixed by surface irregularities or airstream flow disturbances, cooling was not effective in obtaining laminar flow behind the irregularity or disturbances.

Applied Mechanics Reviews

Applied Mechanics Reviews
Author:
Publisher:
Total Pages: 608
Release: 1955
Genre: Mechanics, Applied
ISBN:

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Handbook of Supersonic Aerodynamics

Handbook of Supersonic Aerodynamics
Author: Johns Hopkins University. Applied Physics Laboratory
Publisher:
Total Pages: 372
Release: 1961
Genre: Aerodynamics, Supersonic
ISBN:

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The Influence of Low Wall Temperature on Boundary-layer Transition and Local Heat Transfer on 2-inch-diameter Hemispheres at a Mach Number of 4.95 and a Reynolds Number Per Foot of 73.2 X 106

The Influence of Low Wall Temperature on Boundary-layer Transition and Local Heat Transfer on 2-inch-diameter Hemispheres at a Mach Number of 4.95 and a Reynolds Number Per Foot of 73.2 X 106
Author: Morton Cooper
Publisher:
Total Pages: 42
Release: 1960
Genre: Aerodynamics, Hypersonic
ISBN:

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The Influence of Low Wall Temperature on Boundary-Layer Transition and Local Heat Transfer on 2-Inch-Diameter Hemispheres at a Mach Number of 4.95 and a Reynolds Number Per Foot of 73.2 X 10(exp 6)

The Influence of Low Wall Temperature on Boundary-Layer Transition and Local Heat Transfer on 2-Inch-Diameter Hemispheres at a Mach Number of 4.95 and a Reynolds Number Per Foot of 73.2 X 10(exp 6)
Author: Morton Cooper
Publisher:
Total Pages: 50
Release: 1960
Genre:
ISBN:

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