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
Author :
Publisher :
Total Pages : 32
Release :
ISBN-10 : UIUC:30112106631424
ISBN-13 :
Rating : 4/5 ( Downloads)

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:

DOWNLOAD EBOOK

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:

DOWNLOAD EBOOK

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:

DOWNLOAD EBOOK

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:

DOWNLOAD EBOOK

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:

DOWNLOAD EBOOK

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