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Some Turbulent Boundary Layer Measurements Obtained From The Forebody Of An Airplane At Mach Numbers Up To 172
Download Some Turbulent Boundary Layer Measurements Obtained From The Forebody Of An Airplane At Mach Numbers Up To 172 full books in PDF, epub, and Kindle. Read online Some Turbulent Boundary Layer Measurements Obtained From The Forebody Of An Airplane At Mach Numbers Up To 172 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Analytical, Numerical, and Experimental Results on Turbulent Boundary Layers by : David L. Whitfield
Download or read book Analytical, Numerical, and Experimental Results on Turbulent Boundary Layers written by David L. Whitfield and published by . This book was released on 1976 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes the results of analytical, numerical, and experimental investigations of incompressible and compressible boundary layers. The subjects considered are (1) Laminar and/or turbulent numerical boundary-layer calculations in which the Reynolds stress is related to the turbulent kinetic energy; (2) an analytical investigation of turbulence near a wall which is not founded on classical mixing-length theory; (3) analytical solutions for relating velocity and temperature throughout turbulent boundary layers for nonunity Prandtl numbers; (4) a description of the data reduction of pitot pressure measurements utilizing these analytical results, and (5) the application of the numerical and analytical results to the analysis of turbulent boundary-layer measurements made in the Propulsion Wind Tunnel Facility (PWT).
Book Synopsis Monthly Catalogue, United States Public Documents by :
Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1970 with total page 1730 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Fluctuation Measurements in Supersonic Turbulent Boundary Layers by : Alan. L. Kistler
Download or read book Fluctuation Measurements in Supersonic Turbulent Boundary Layers written by Alan. L. Kistler and published by . This book was released on 1958 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Flight Investigation of the Effect of Shape and Thickness of the Boundary Layer on the Pressure Distribution in the Presence of Shock by : Eziaslav N. Harrin
Download or read book A Flight Investigation of the Effect of Shape and Thickness of the Boundary Layer on the Pressure Distribution in the Presence of Shock written by Eziaslav N. Harrin and published by . This book was released on 1952 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in flight at free-stream Mach numbers up to about 0.77 to determine the effect of a laminar boundary layer and thin and thick turbulent boundary layers on the chordwise pressure distribution over an airfoil in the presence of shock at full-scale Reynolds numbers. Boundary-layer and pressure-distribution measurements were made on a short-span airfoil built around ar wing of a fighter plane. Boundary-layer Reynolds numbers (based on momentum thickness and flow parameters at the outer edge of the boundary layer) were about 3,000 for the laminar boundary layer and 10,000 for the thickest turbulent boundary layer with local Mach numbers ranging up to 1.3 and chord Reynolds numbers up to about 21,000,000.
Book Synopsis Boundary Layer Effects by : Anthony W. Fiore
Download or read book Boundary Layer Effects written by Anthony W. Fiore and published by . This book was released on 1978 with total page 962 pages. Available in PDF, EPUB and Kindle. Book excerpt: In 1975 the U.S. Air Force and the Federal Republic of Germany signed a Data Exchange Agreement numbered AF-75-G-7440 entitled 'Viscous and Interacting Flow Fields.' The purpose was to exchange data in the area of boundary layer research. It includes both experimental and theoretical boundary layer research at speeds from subsonic to hypersonic Mach numbers in the presence of laminar, transitional, and turbulent boundary layers. The main effort in recent years has been on turbulent boundary layers, both attached and separated in the presence of such parameters as pressure gradients, wall temperature, surface roughness, etc. In the United States the research was conducted in various Department of Defense, NASA, aircraft corporations, and various university laboratories. In the Federal Republic of Germany it was carried out within the various DFVLR, industrial, and university research centers.
Book Synopsis Turbulent Boundary-layer Studies at High Reynolds Numbers at Mach Numbers Between 0.2 and 2.8 by : Kenneth George Winter
Download or read book Turbulent Boundary-layer Studies at High Reynolds Numbers at Mach Numbers Between 0.2 and 2.8 written by Kenneth George Winter and published by . This book was released on 1970 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Turbulent Boundary Layers Over Nonstationary Plane Boundaries by : Alan T. Roper
Download or read book Turbulent Boundary Layers Over Nonstationary Plane Boundaries written by Alan T. Roper and published by . This book was released on 1978 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Boundary-layer Measurements in Accelerated Flows Near Mach 1 by : Howard L. Wesoky
Download or read book Boundary-layer Measurements in Accelerated Flows Near Mach 1 written by Howard L. Wesoky and published by . This book was released on 1967 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Turbulent Boundary-Layer Studies at high Reynolds numbers at Mach numbers between 0,2 and 2,8 by : K. G. Winter
Download or read book Turbulent Boundary-Layer Studies at high Reynolds numbers at Mach numbers between 0,2 and 2,8 written by K. G. Winter and published by . This book was released on 1973 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Compressible Turbulent Boundary Layer with Surface Mass Transfer by : Fred Culick
Download or read book The Compressible Turbulent Boundary Layer with Surface Mass Transfer written by Fred Culick and published by . This book was released on 1960 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Study of the Turbulent Boundary Layer at Mach 15 and 19.8 in a Conical Nozzle by : Edgard Backx
Download or read book Experimental Study of the Turbulent Boundary Layer at Mach 15 and 19.8 in a Conical Nozzle written by Edgard Backx and published by . This book was released on 1974 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Calculation of the Turbulent Boundary Layer and of Transition on a Plane Plate by : René Hirsch
Download or read book Calculation of the Turbulent Boundary Layer and of Transition on a Plane Plate written by René Hirsch and published by . This book was released on 1967 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Behavior of Turbulent Boundary Layers on Curved Convex Walls by : Hans Schmidbauer
Download or read book Behavior of Turbulent Boundary Layers on Curved Convex Walls written by Hans Schmidbauer and published by . This book was released on 1936 with total page 570 pages. Available in PDF, EPUB and Kindle. Book excerpt: The system of linear differential equations which indicated the approach of separation and the so-called "boundary-layer thickness" by Gruschwitz is extended in this report to include the case where the friction layer is subject to centrifugal forces. Evaluation of the data yields a strong functional dependence of the momentum change and wall drag on the boundary-layer thickness radius of curvature ratio for the wall. It is further shown that the transition from laminar to turbulent flow occurs at somewhat higher Reynolds Numbers at the convex wall than at the flat plate, due to the stabilizing effect of the centrifugal forces.
Book Synopsis Turbulence, Heat-transfer, and Boundary Layer Measurements in a Conical Nozzle with a Controlled Inlet Velocity Profile by : Donald R. Boldman
Download or read book Turbulence, Heat-transfer, and Boundary Layer Measurements in a Conical Nozzle with a Controlled Inlet Velocity Profile written by Donald R. Boldman and published by . This book was released on 1966 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Distributed Three-dimensional Roughness and Surface Cooling on Boundary-layer Transition and Lateral Spread of Turbulence at Supersonic Speeds by : Albert L. Braslow
Download or read book Effect of Distributed Three-dimensional Roughness and Surface Cooling on Boundary-layer Transition and Lateral Spread of Turbulence at Supersonic Speeds written by Albert L. Braslow and published by . This book was released on 1959 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack by : Donald M. Kuehn
Download or read book Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack written by Donald M. Kuehn and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Tech Briefs written by and published by . This book was released on 1990 with total page 466 pages. Available in PDF, EPUB and Kindle. Book excerpt:
