Comparison of Secondary Flows and Boundary-layer Accumulations in Several Turbine Nozzles 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 Comparison of Secondary Flows and Boundary-layer Accumulations in Several Turbine Nozzles PDF full book. Access full book title Comparison of Secondary Flows and Boundary-layer Accumulations in Several Turbine Nozzles by Milton G. Kofskey. Download full books in PDF and EPUB format.
Author: Milton G. Kofskey Publisher: ISBN: Category : Air flow Languages : en Pages : 68
Book Description
An investigation of secondary-flow loss cores originating in turbine nozzle blade passages was conducted by means of flow visualization studies and detailed flow measurements. The degree of which blade surface velocity profiles affect the magnitude and concentration of loss cores was investigated by comparing three nozzle blade configurations.
Author: Milton G. Kofskey Publisher: ISBN: Category : Air flow Languages : en Pages : 68
Book Description
An investigation of secondary-flow loss cores originating in turbine nozzle blade passages was conducted by means of flow visualization studies and detailed flow measurements. The degree of which blade surface velocity profiles affect the magnitude and concentration of loss cores was investigated by comparing three nozzle blade configurations.
Author: Riley O. Miller Publisher: ISBN: Category : Combustion Languages : en Pages : 644
Book Description
At -40 degrees F, several blends of aromatic amines with triethylamine show promise as ignitor fuels with mixed acid (nitric acid plus sulfuric acid) and red fuming nitric acid} and some of these fuels may be useful also with white fuming nitric acid.
Author: Warren J. Whitney Publisher: ISBN: Category : Aerofoils Languages : en Pages : 716
Book Description
Mass-flow tables for ratios of specific heats of 1.3 and 1.4 are presented for the entire range of critical velocity ratio. The tables enable a quick and accurate determination of the integrated average specific mass flow across a region where the end-point velocities are known, commensurate with the assumptions that the total state is constant and the static pressure varies linearly between the two velocities. A numerical example is included to illustrate the use of the tables. All quantities are in nondimensional form and are tabulated sgainst critical velocity ratio. The tables include specific-mass-flow parameter and ratio of static to total pressure.
Author: Milton G. Kofskey
Author: Milton G. Kofskey
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Author: Albert P. Martina
Author: 
Author: Riley O. Miller
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: Warren J. Whitney
Author: