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Author : Amruthkiran Hegde
Publisher :
ISBN 13 :
Total Pages : 69 pages
Book Rating : 4.:/5 (96 download)
Download or read book Experimental Investigation Into Shock Induced Corner Boundary Layer Separation written by Amruthkiran Hegde and published by . This book was released on 2015 with total page 69 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Morgan Lee Funderburk
Publisher :
ISBN 13 :
Total Pages : 90 pages
Book Rating : 4.:/5 (963 download)
Download or read book Experimental Investigation of Primary and Corner Shock Boundary Layer Interactions at Mild and Increasing Back Pressure Ratios written by Morgan Lee Funderburk and published by . This book was released on 2016 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Eugene S. Love
Publisher :
ISBN 13 :
Total Pages : 702 pages
Book Rating : 4.F/5 ( download)
Download or read book Pressure Rise Associated with Shock-induced Boundary-layer Separation written by Eugene S. Love and published by . This book was released on 1955 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt: Some recent contributions to the problem of shock-induced separation of the boundary layer are examined, and additional analytical and experimental results are presented. The probable ranges of pressure rises and flow deflections associated with separation are indicated. Consideration is given to the effects of Mach number, adverse pressure gradient, and Reynolds number for laminar boundary layers and to the effects of Mach number, Reynolds number, and ratio of sepcific heats for turbulent boundary layers.
Author : D. D'Ambrosio
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (317 download)
Download or read book Shock-Induced Separated Structures in Symmetric Corner Flows written by D. D'Ambrosio and published by . This book was released on 1995 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Coleman duP. Donaldson
Publisher :
ISBN 13 :
Total Pages : 2 pages
Book Rating : 4.3/5 (91 download)
Download or read book Study of the Pressure Rise Across Shock Waves Required to Separate Laminar and Turbulent Boundary Layers written by Coleman duP. Donaldson and published by . This book was released on 1952 with total page 2 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Piotr Doerffer
Publisher : Springer Science & Business Media
ISBN 13 : 3642030041
Total Pages : 350 pages
Book Rating : 4.6/5 (42 download)
Download or read book Unsteady Effects of Shock Wave induced Separation written by Piotr Doerffer and published by Springer Science & Business Media. This book was released on 2010-11-25 with total page 350 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume contains description of experimental and numerical results obtained in the UFAST project. The goal of the project was to generate experiment data bank providing unsteady characteristics of the shock boundary layer interaction. The experiments concerned basic-reference cases and the cases with application of flow control devices. Obtained new data bank have been used for the comparison with available simulation techniques, starting from RANS, through URANS, LES and hybrid RANS-LES methods. New understanding of flow physics as well as ability of different numerical methods in the prediction of such unsteady flow phenomena will be discussed.
Author :
Publisher :
ISBN 13 :
Total Pages : 23 pages
Book Rating : 4.:/5 (742 download)
Download or read book Experimental Investigation of Upstream Boundary Layer Acceleration on Unsteadiness of Shock-Induced Separation written by and published by . This book was released on 2003 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: This project was aimed at understanding the fundamental cause of the low frequency unsteadiness present in shock-induced turbulent separated flows. A new multi-camera, multi-laser PIV system was used to capture wide-field images of the velocity field in a Mach 2 compression ramp interaction. The PIV was acquired simultaneously with fast-response pressure measurements to identify the shock-foot location at the same time that the PIV data were captured. The measurements showed that the global structure of the interaction was substantially different depending on the location of the separation shock foot. For example, when the shock is upstream, the scale of the separated flow, the velocity fluctuations and the domain of perturbed flow, are all substantially larger than when the shock-foot is located downstream. Most importantly, a clear correlation was observed between the thickness and velocity profile in the upstream boundary layer and the shock foot position. A new technique for measuring the upstream boundary layer acceleration by using two-frame time-sequenced PIV was also developed. This involved developing new hardware and software tools, and conducting preliminary calibration experiments. This work has shown the feasibility of correlating the upstream acceleration to the shock motion and these measurements will be made in future work.
Author : C. C. Sun
Publisher :
ISBN 13 :
Total Pages : 916 pages
Book Rating : 4.:/5 (317 download)
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.
Author : Jeffrey David Brown
Publisher :
ISBN 13 :
Total Pages : 268 pages
Book Rating : 4.:/5 (29 download)
Download or read book Two-component LDV Investigation of Shock-related Turbulent Boundary Layer Separation with Increasing Three-dimensionality written by Jeffrey David Brown and published by . This book was released on 1986 with total page 268 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Paul K. Berg
Publisher :
ISBN 13 :
Total Pages : 394 pages
Book Rating : 4.:/5 (295 download)
Download or read book An Experimental Investigation of Unsteady Periodic Boundary Layer Separation written by Paul K. Berg and published by . This book was released on 1993 with total page 394 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : C. Herbert Law
Publisher :
ISBN 13 :
Total Pages : 120 pages
Book Rating : 4.3/5 (91 download)
Download or read book Two-dimensional Compression Corner and Planar Shock Wave Interactions with a Supersonic, Turbulent Boundary Layer written by C. Herbert Law and published by . This book was released on 1975 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Charles Keith Cretcher
Publisher :
ISBN 13 :
Total Pages : 102 pages
Book Rating : 4.:/5 (57 download)
Download or read book The Pressure Rise Associated with Shock-induced Laminar Boundary Layer Separation written by Charles Keith Cretcher and published by . This book was released on 1963 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Piotr Doerffer
Publisher : Springer Nature
ISBN 13 : 3030474615
Total Pages : 540 pages
Book Rating : 4.0/5 (34 download)
Download or read book Transition Location Effect on Shock Wave Boundary Layer Interaction written by Piotr Doerffer and published by Springer Nature. This book was released on 2020-07-30 with total page 540 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book presents experimental and numerical findings on reducing shock-induced separation by applying transition upstream the shock wave. The purpose is to find out how close to the shock wave the transition should be located in order to obtain favorable turbulent boundary layer interaction. The book shares findings obtained using advanced flow measurement methods and concerning e.g. the transition location, boundary layer characteristics, and the detection of shock wave configurations. It includes a number of experimental case studies and CFD simulations that offer valuable insights into the flow structure. It covers RANS/URANS methods for the experimental test section design, as well as more advanced techniques, such as LES, hybrid methods and DNS for studying the transition and shock wave interaction in detail. The experimental and numerical investigations presented here were conducted by sixteen different partners in the context of the TFAST Project. The general focus is on determining if and how it is possible to improve flow performance in comparison to laminar interaction. The book mainly addresses academics and professionals whose work involves the aerodynamics of internal and external flows, as well as experimentalists working with compressible flows. It will also be of benefit for CFD developers and users, and for students of aviation and propulsion systems alike.
Author : Stanley Andrew Skebe
Publisher :
ISBN 13 :
Total Pages : 1482 pages
Book Rating : 4.:/5 (11 download)
Download or read book Experimental Investigation of Two Dimensional Shock Boundary Layer Interactions written by Stanley Andrew Skebe and published by . This book was released on 1983 with total page 1482 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Hyun D. Kim
Publisher :
ISBN 13 :
Total Pages : 14 pages
Book Rating : 4.:/5 (317 download)
Download or read book Experimental Investigation of Crossing Shock Wave-Turbulent Boundary Layer-Bleed Interaction written by Hyun D. Kim and published by . This book was released on 1996 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Pairoj Chevasuwan
Publisher :
ISBN 13 :
Total Pages : 102 pages
Book Rating : 4.:/5 (392 download)
Download or read book An Experimental Study of Turbulent Boundary-layer Separation with Upstream Disturbance written by Pairoj Chevasuwan and published by . This book was released on 1977 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Oktay Ozcan
Publisher :
ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.:/5 (381 download)
Download or read book An Experimental Investigation of Three-dimensional Boundary Layer Separation in Supersonic Flow Past a Circular Cylinder on a Flat Plate written by Oktay Ozcan and published by . This book was released on 1982 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
