EBookClubs

Read Books & Download eBooks Full Online

EBookClubs

Read Books & Download eBooks Full Online

Book Turbulent Boundary Layer Displacement Effects in Hypersonic Flow

Download or read book Turbulent Boundary Layer Displacement Effects in Hypersonic Flow written by and published by . This book was released on 1967 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Boundary layer Displacement Effects in Air at Mach Numbers of 6 8 and 9 6

Download or read book Boundary layer Displacement Effects in Air at Mach Numbers of 6 8 and 9 6 written by Mitchel H. Bertram and published by . This book was released on 1959 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Viscous Hypersonic Flow

Download or read book Viscous Hypersonic Flow written by William H. Dorrance and published by Courier Dover Publications. This book was released on 2017-05-22 with total page 353 pages. Available in PDF, EPUB and Kindle. Book excerpt: Designed for advanced undergraduate and graduate courses in modern boundary-layer theory, this frequently cited work offers a self-contained treatment of theories for treating laminar and turbulent boundary layers of reacting gas mixtures. 1962 edition.

Book The Flow Field Over Blunted Flat Plates and Its Effect on Turbulent Boundary layer Growth and Heat Transfer at a Mach Number of 4 7

Download or read book The Flow Field Over Blunted Flat Plates and Its Effect on Turbulent Boundary layer Growth and Heat Transfer at a Mach Number of 4 7 written by Thorval Tendeland and published by . This book was released on 1961 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Analysis of the Three dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow

Download or read book Analysis of the Three dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow written by John C. Adams and published by . This book was released on 1972 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analytical approach toward numerical calculation of the three-dimensional turbulent boundary layer on a sharp cone at incidence under supersonic and hypersonic flow conditions is presented. The theoretical model is based on implicit finite-difference integration of the governing three-dimensional turbulent boundary-layer equations in conjunction with a three-dimensional scalar eddy-viscosity model of turbulence. Comparison is made of present theory with detailed experimental measurements of the three-dimensional turbulent boundary-layer structure (velocity and temperature profiles), the surface streamline direction (obtained via an oil-flow technique) and surface heat-transfer rate.

Book Some Heat Transfer Problems in Hypersonic Flow

Download or read book Some Heat Transfer Problems in Hypersonic Flow written by Antonio Ferri and published by . This book was released on 1959 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Documentation of Two  and Three dimensional Hypersonic Shock Wave turbulent Boundary Layer Interaction Flows

Download or read book Documentation of Two and Three dimensional Hypersonic Shock Wave turbulent Boundary Layer Interaction Flows written by Marvin I. Kussoy and published by . This book was released on 1989 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Measurements of Upstream History Effects in Compressible Turbulent Boundary Layers

Download or read book Measurements of Upstream History Effects in Compressible Turbulent Boundary Layers written by David F. Gates and published by . This book was released on 1973 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report describes an experimental study of compressible turbulent boundary layers for which the upstream history was systematically varied. A series of experiments was conducted using both a supersonic half nozzle and a conventional flat plate for which the nozzle throat and flat plate leading edge can be temperature controlled. The supersonic nozzle provided a favorable upstream pressure gradient together with a controlled thermal history at the throat. The flat plate provided upstream temperature control with no pressure history. Velocity and temperature profile and heat-transfer measurements were made in a downstream region of zero-pressure-gradient and constant wall temperature. (Modified author abstract).

Book Hypersonic Inviscid Flow

    Book Details:
  • Author : Wallace D. Hayes
  • Publisher : Courier Corporation
  • Release : 2012-07-13
  • ISBN : 0486160483
  • Pages : 628 pages

Download or read book Hypersonic Inviscid Flow written by Wallace D. Hayes and published by Courier Corporation. This book was released on 2012-07-13 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt: Unified, self-contained view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer; appropriate for graduate-level courses in hypersonic flow theory. 1966 edition.

Book An Approximate Method for Determining the Displacement Effects and Viscous Drag of Laminar Boundary Layers in Two dimensional Hypersonic Flow

Download or read book An Approximate Method for Determining the Displacement Effects and Viscous Drag of Laminar Boundary Layers in Two dimensional Hypersonic Flow written by Mitchel H. Bertram and published by . This book was released on 1952 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: