Turbulent Boundary Layer Separation Induced By Flares On Cylinders At Zero Angle Of Attack

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Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack

Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack
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Total Pages : 32
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ISBN-10 : UIUC:30112106631424
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Book Synopsis Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack by : Donald M. Kuehn

Download or read book Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack written by Donald M. Kuehn and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:


Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack Related Books

Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack
Language: en
Pages: 32
Authors: Donald M. Kuehn
Categories: Noses (Space vehicles)
Type: BOOK - Published: 1961 - Publisher:

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Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack
Language: en
Pages: 26
Authors: Donald M. Kuehn
Categories:
Type: BOOK - Published: 1961 - Publisher:

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Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack
Language: en
Pages: 36
Authors: Donald M. Kuehn
Categories: Noses (Space vehicles)
Type: BOOK - Published: 1961 - Publisher:

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Separation caused by the pressure rise induced by flares has been experimentally investigated in the Mach number range of 1.5 to 5.0 and in the Reynolds number
Laminar Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack
Language: en
Pages: 28
Authors: Donald M. Kuehn
Categories: Angle of attack (Aerodynamics)
Type: BOOK - Published: 1962 - Publisher:

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Hypersonic-turbulent Boundary-layer Separation Over a Cone-cylinder-flare Configuration
Language: en
Pages: 56
Authors: Arnold Polak
Categories: Aerodynamics, Hypersonic
Type: BOOK - Published: 1969 - Publisher:

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Results of a study of hypersonic-turbulent boundary-layer separation over axisymmetric bodies are presented. Pressure, heat-transfer and flow visualization data