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A Study Of The Interaction Between A Glancing Shock Wave And A Turbulent Boundary Layer
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Book Synopsis A Study of the Interaction Between a Glancing Shock Wave and a Turbulent Boundary Layer by : H. Kubota
Download or read book A Study of the Interaction Between a Glancing Shock Wave and a Turbulent Boundary Layer written by H. Kubota and published by . This book was released on 1980 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Study of the Interaction Between a Glancing Shock Wave and a Turbulent Boundary Layer by : A. Hussain
Download or read book A Study of the Interaction Between a Glancing Shock Wave and a Turbulent Boundary Layer written by A. Hussain and published by . This book was released on 1985 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of the Glancing Interaction Between a Shock Wave and a Turbulent Boundary Layer by : Aeronautical Research Council (Great Britain)
Download or read book An Experimental Study of the Glancing Interaction Between a Shock Wave and a Turbulent Boundary Layer written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1961 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of the Glancing Interaction Between a Shock Wave and a Turbulent Boundary Layer by :
Download or read book An Experimental Study of the Glancing Interaction Between a Shock Wave and a Turbulent Boundary Layer written by and published by . This book was released on 1961 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Shock Wave-Boundary-Layer Interactions by : Holger Babinsky
Download or read book Shock Wave-Boundary-Layer Interactions written by Holger Babinsky and published by Cambridge University Press. This book was released on 2011-09-12 with total page 481 pages. Available in PDF, EPUB and Kindle. Book excerpt: Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722499792 Total Pages :98 pages Book Rating :4.4/5 (997 download)
Book Synopsis Interaction of Two Glancing, Crossing Shock Waves with a Turbulent Boundary-Layer at Various Mach Numbers by : National Aeronautics and Space Administration (NASA)
Download or read book Interaction of Two Glancing, Crossing Shock Waves with a Turbulent Boundary-Layer at Various Mach Numbers written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-08 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt: A preliminary experimental investigation was conducted to study two crossing, glancing shock waves of equal strengths, interacting with the boundary-layer developed on a supersonic wind tunnel wall. This study was performed at several Mach numbers between 2.5 and 4.0. The shock waves were created by fins (shock generators), spanning the tunnel test section, that were set at angles varying from 4 to 12 degrees. The data acquired are wall static pressure measurements, and qualitative information in the form of oil flow and schlieren visualizations. The principle aim is two-fold. First, a fundamental understanding of the physics underlying this flow phenomena is desired. Also, a comprehensive data set is needed for computational fluid dynamic code validation. Results indicate that for small shock generator angles, the boundary-layer remains attached throughout the flow field. However, with increasing shock strengths (increasing generator angles), boundary layer separation does occur and becomes progressively more severe as the generator angles are increased further. The location of the separation, which starts well downstream of the shock crossing point, moves upstream as shock strengths are increased. At the highest generator angles, the separation appears to begin coincident with the generator leading edges and engulfs most of the area between the generators. This phenomena occurs very near the 'unstart' limit for the generators. The wall pressures at the lower generator angles are nominally consistent with the flow geometries (i.e. shock patterns) although significantly affected by the boundary-layer upstream influence. As separation occurs, the wall pressures exhibit a gradient that is mainly axial in direction in the vicinity of the separation. At the limiting conditions the wall pressure gradients are primarily in the axial direction throughout. Hingst, Warren R. and Williams, Kevin E. Glenn Research Center...
Book Synopsis Interaction of Two Glancing, Crossing Shock Waves with a Turbulent Boundary-layer at Various Mach Numbers by :
Download or read book Interaction of Two Glancing, Crossing Shock Waves with a Turbulent Boundary-layer at Various Mach Numbers written by and published by . This book was released on 1991 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A study of the interaction between the turbulent boundary-layer and the shock wave upstream of fins of varying yaw and sweep in supersonic flow by : James Wilbert Cutbirth
Download or read book A study of the interaction between the turbulent boundary-layer and the shock wave upstream of fins of varying yaw and sweep in supersonic flow written by James Wilbert Cutbirth and published by . This book was released on 1973 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves by : Earl C. Watson
Download or read book Investigation of Laminar and Turbulent Boundary Layers Interacting with Externally Generated Shock Waves written by Earl C. Watson and published by . This book was released on 1969 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt: Laminar and turbulent boundary layer interactions with externally generated shock waves.
Book Synopsis The Interaction Between an Oblique Shock-wave and a Turbulent Boundary-layer by : O. Bardsley
Download or read book The Interaction Between an Oblique Shock-wave and a Turbulent Boundary-layer written by O. Bardsley and published by . This book was released on 1950 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Detailed Study of the Interaction of a 140 Shock Wave with a Turbulent Boundary Layer at M by : I. E. Vas
Download or read book A Detailed Study of the Interaction of a 140 Shock Wave with a Turbulent Boundary Layer at M written by I. E. Vas and published by . This book was released on 1955 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Detailed Study of the Interaction of a 14° Shock Wave with a Turbulent Boundary Layer at M by : Irwin E. Vas
Download or read book A Detailed Study of the Interaction of a 14° Shock Wave with a Turbulent Boundary Layer at M written by Irwin E. Vas and published by . This book was released on 1955 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Study of Shock Wave Turbulent Boundary Layer Interaction at M by : S.M. Bogdonoff
Download or read book A Study of Shock Wave Turbulent Boundary Layer Interaction at M written by S.M. Bogdonoff and published by . This book was released on 1953 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Interaction of a Shock Wave with a Turbulent Boundary Layer at M by : I.E. Vas
Download or read book Interaction of a Shock Wave with a Turbulent Boundary Layer at M written by I.E. Vas and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Interaction of a Shock Wave and a Turbulent Boundary Layer in by : William Russell Seebaugh
Download or read book Investigation of the Interaction of a Shock Wave and a Turbulent Boundary Layer in written by William Russell Seebaugh and published by . This book was released on 1968 with total page 920 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Shock Wave-turbulent Boundary Layer Interactions with and Without Boundary Layer Suction by : C. C. Sun
Download or read book An Experimental Investigation of Shock Wave-turbulent Boundary Layer Interactions with and Without Boundary Layer Suction written by C. C. Sun and published by . This book was released on 1977 with total page 916 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tabulated data from a series of experimental studies of the interaction of a shock wave with a turbulent boundary layer in axisymmetric flow configurations is presented. The studies were conducted at the walls of circular wind tunnels and on the cylindrical centerbody of an annular flow channel. Detailed pitot pressure profiles and wall static pressure profiles upstream of, within and downstream of the interaction region are given. Results are presented for flows at nominal freestream Mach Numbers of 2, 3 and 4. For studies at the tunnel sidewalls, the shock waves were produced by conical shock generators mounted on the centerline of the wind tunnel at zero angle of attack. The annular ring generator was used to produce the shock wave at the centerbody of the annular flow channel. The effects of boundary layer bleed were examined in the investigation. Both bleed rate and bleed location were studied. Most of the bleed studies were conducted with bleed holes drilled normal to the wall surface but the effects of slot suction were also examined. A summary of the principal results and conclusions is given.
Book Synopsis The Interaction Between a Weak Normal Shock Wave and a Turbulent Boundary Layer by : Aeronautical Research Council
Download or read book The Interaction Between a Weak Normal Shock Wave and a Turbulent Boundary Layer written by Aeronautical Research Council and published by . This book was released on 1959 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: