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.
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).
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).
Author: David L. Brott Publisher: ISBN: Category : Flow meters Languages : en Pages : 60
Book Description
This report presents the experimental investigation of surface Pitot probe in both subsonic and supersonic flow. The effect of heat transfer on the results was also investigated in supersonic flow. (Author).
Author: David L. Brott
Author: David L. Brott
Author: David L. Brott
Author: 
Author: 
Author: 
Author: 
Author: Robert L. P. Voisinet
Author: 
Author: 
Author: United States. National Advisory Committee for Aeronautics