Some Effects of Leading-edge Sweep on Boundary-layer Transition at Supersonic Speeds

Some Effects of Leading-edge Sweep on Boundary-layer Transition at Supersonic Speeds
Author: Gary T. Chapman
Publisher:
Total Pages: 38
Release: 1961
Genre: Fluid mechanics
ISBN:

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Some Effects of Leading-edge Sweep on Boundary-layer Transition at Supersonic Speeds
Language: en
Pages: 38
Authors: Gary T. Chapman
Categories: Fluid mechanics
Type: BOOK - Published: 1961 - Publisher:

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Some Effects of Leading-edge Sweep on Boundary-layer Transition at Supersonic Speeds
Language: en
Pages: 1
Authors: Gary T. Chapman
Categories:
Type: BOOK - Published: 1961 - Publisher:

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The effects of crossflow and shock strength on transition of the laminar boundary layer behind a swept leading edge have been investigated analytically and with
Effects of Mach Number, Leading Edge Bluntness and Sweep on Boundary-layer Transition on a Flat Plate
Language: en
Pages: 36
Authors: Don W. Jillie
Categories: Fluid mechanics
Type: BOOK - Published: 1961 - Publisher:

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Boundary-layer Transition at Supersonic Speeds
Language: en
Pages: 35
Authors: George M. Low
Categories: Boundary layer
Type: BOOK - Published: 1956 - Publisher:

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The effects of leading-edge blunting on two-dimensional surfaces and surface cooling can be predicted adequately by existing theories, at least in the moderate
Boundary-layer Transition Study of Several Pointed Bodies of Revolution at Supersonic Speeds
Language: en
Pages: 76
Authors: William A. Cassels
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1970 - Publisher:

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Boundary-layer transition by the sublimation and impact-pressure techniques and force tests have been performed on three Haack-Adams bodies of revolution of fin