An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient PDF full book. Access full book title An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient by David L. Brott. Download full books in PDF and EPUB format.

An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient

An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient PDF Author: David L. Brott
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 104

Book Description
The paper describes the results of a detailed experimental investigation of a two-dimensional turbulent boundary layer in a favorable pressure gradient where the free-stream Mach number varied from 3.8 to 4.6 and the ratio of wall to adiabatic-wall temperature has a nominal value of 0.82. Detailed profile measurements were made with pressure and temperature probes; skin friction was measured directly with a shear balance. The velocity- and temperature-profile results were compared with zero pressure gradient and incompressible results. The skin-friction data were correlated with momentum-thickness Reynolds number and pressure-gradient parameter. (Author).

An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient

An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient PDF Author: David L. Brott
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 104

Book Description
The paper describes the results of a detailed experimental investigation of a two-dimensional turbulent boundary layer in a favorable pressure gradient where the free-stream Mach number varied from 3.8 to 4.6 and the ratio of wall to adiabatic-wall temperature has a nominal value of 0.82. Detailed profile measurements were made with pressure and temperature probes; skin friction was measured directly with a shear balance. The velocity- and temperature-profile results were compared with zero pressure gradient and incompressible results. The skin-friction data were correlated with momentum-thickness Reynolds number and pressure-gradient parameter. (Author).

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 994

Book Description


Report

Report PDF Author: United States. National Bureau of Standards
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 336

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1148

Book Description


Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 520

Book Description


NBS Special Publication

NBS Special Publication PDF Author:
Publisher:
ISBN:
Category : Weights and measures
Languages : en
Pages : 1164

Book Description


An Experimental Investigation of the Structure of a Turbulent Reattaching Flow Behind a Backward-facing Step

An Experimental Investigation of the Structure of a Turbulent Reattaching Flow Behind a Backward-facing Step PDF Author: Stephen W. Pronchick
Publisher:
ISBN:
Category : Turbulent boundary layer
Languages : en
Pages : 180

Book Description
The structure of a turbulent reattaching flow behind a backward-facing step was studied experimentally in a low-velocity water channel, in order to observe the physical structure of the flow and to better understand the relation.

Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 912

Book Description


U.S. Government Research & Development Reports

U.S. Government Research & Development Reports PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 212

Book Description


Report

Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962

Book Description