An Experimental Investigation of a Two-Dimensional, Self-Similar, Supersonic Turbulent Mixing Layer with Zero Pressure Gradient

An Experimental Investigation of a Two-Dimensional, Self-Similar, Supersonic Turbulent Mixing Layer with Zero Pressure Gradient
Author :
Publisher :
Total Pages : 39
Release :
ISBN-10 : OCLC:227569455
ISBN-13 :
Rating : 4/5 (55 Downloads)

Book Synopsis An Experimental Investigation of a Two-Dimensional, Self-Similar, Supersonic Turbulent Mixing Layer with Zero Pressure Gradient by : Hideo Ikawa

Download or read book An Experimental Investigation of a Two-Dimensional, Self-Similar, Supersonic Turbulent Mixing Layer with Zero Pressure Gradient written by Hideo Ikawa and published by . This book was released on 1973 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effect of compressibility on the mixing layer was investigated at Mach number 2.47. Pitot pressure, static pressure and hot-wire surveys were made to investigate the mean flow and the fluctuation quantities. Similarities between supersonic and incompressible mixing layers are observed in normalized velocity profile, normalized power spectral density distribution and convection velocity distribution. Spreading rate, normalized shear stress and velocity fluctuation were found to be appreciably smaller than the respective incompressible results; e.g., the momentum thickness growth rates are 0.0073 and 0.035 for supersonic and incompressible flows, respectively. The difference between free and wall-bounded mixing layers is discussed. Development of turbulence structure of mixing layer with increasing Reynolds number was also investigated. (Author).


An Experimental Investigation of a Two-Dimensional, Self-Similar, Supersonic Turbulent Mixing Layer with Zero Pressure Gradient Related Books

An Experimental Investigation of a Two-Dimensional, Self-Similar, Supersonic Turbulent Mixing Layer with Zero Pressure Gradient
Language: en
Pages: 39
Authors: Hideo Ikawa
Categories:
Type: BOOK - Published: 1973 - Publisher:

DOWNLOAD EBOOK

The effect of compressibility on the mixing layer was investigated at Mach number 2.47. Pitot pressure, static pressure and hot-wire surveys were made to invest
Research in Progress
Language: en
Pages: 652
Authors:
Categories: Military research
Type: BOOK - Published: 1975 - Publisher:

DOWNLOAD EBOOK

Scientific and Technical Aerospace Reports
Language: en
Pages: 704
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1995 - Publisher:

DOWNLOAD EBOOK

An Experimental Investigation of a Zero Pressure Gradient Two Dimensional Turbulent Boundary Layer
Language: en
Pages: 78
Applied Mechanics Reviews
Language: en
Pages: 620
Authors:
Categories: Mechanics, Applied
Type: BOOK - Published: 1974 - Publisher:

DOWNLOAD EBOOK