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Download or read book Experimental Investigation of Shock Wave and Boundary Layer Interaction Near Convex Corners in Hypersonic Flow written by and published by . This book was released on 1997 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Sohail Mohammed
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (133 download)
Download or read book Experimental Investigation of Shock Wave and Boundary Layer Interaction Near Convex Corners in Hypersonic Flow written by Sohail Mohammed and published by . This book was released on 1997 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The hypersonic impulse gun tunnel at the UTIAS was used to experimentally investigate the interaction between an oblique shock wave and boundary layer near convex corners in hypersonic flow. Experiments were conducted in two phases. The first phase involved tunnel test operating conditions that presumably developed turbulent boundary layer on the model surface in Mach 7.2 flow. Schlieren photographs indicated that it was not possible to conclude that the boundary layer developed was, in fact, turbulent. The second phase of the program included preliminary investigation of shock-laminar boundary layer interaction near rounded convex conners. As a first step, experiments were repeated to validate previously documented results achieved at the current facility. Surface static pressure measurements and Schlieren photographs were taken to investigate interaction near a 5 degrees convex corner. Results obtained in this phase supported the repeatable characteristics of the facility.
Author : R. J. Hawboldt
Publisher :
ISBN 13 :
Total Pages : 12 pages
Book Rating : 4.:/5 (977 download)
Download or read book Experimental Study of Shock Wave and Hypersonic Boundary Layer Interactions Near a Convex Corner written by R. J. Hawboldt and published by . This book was released on 1993 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert John Hawboldt
Publisher :
ISBN 13 :
Total Pages : 262 pages
Book Rating : 4.:/5 (224 download)
Download or read book An Experimental Study of Shock Wave and Boundary Layer Interactions Near a Convex Corner written by Robert John Hawboldt and published by . This book was released on 1993 with total page 262 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Thomas Johani
Publisher :
ISBN 13 :
Total Pages : 142 pages
Book Rating : 4.:/5 (379 download)
Download or read book An Experimental Investigation of Boundary Layer Expansion Around a Convex Corner in Supersonic Flow written by Thomas Johani and published by . This book was released on 1968 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Ömer Haldun Ünalmış
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (85 download)
Download or read book An Experimental Investigation of Shock-wave/boundary-layer Interaction Induced by Compression Corners & Sharp Fins written by Ömer Haldun Ünalmış and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : C. Nebbeling
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (256 download)
Download or read book An Experimental Investigation of the Interaction Between a Shock Wave and a Turbulent Boundary Layer on a Convex Wall written by C. Nebbeling and published by . This book was released on 1984 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722388287
Total Pages : 66 pages
Book Rating : 4.3/5 (882 download)
Download or read book Experimental Studies of Hypersonic Shock-Wave Boundary-Layer Interactions written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-06 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two classes of shock-wave boundary-layer interactions were studied experimentally in a shock tunnel in which a low Reynolds number, turbulent flow at Mach 8 was developed on a cold, flat test surface. The two classes of interactions were: (1) a swept interaction generated by a wedge ('fin') mounted perpendicularly on the flat plate; and (2) a two-dimensional, unseparated interaction induced by a shock impinging near an expansion corner. The swept interaction, with wedge angles of 5-20 degrees, was separated and there was also indication that the strongest interactions prossessed secondary separation zones. The interaction spread out extensively from the inviscid shock location although no indication of quasi-conical symmetry was evident. The surface pressure from the upstream influence to the inviscid shock was relatively low compared to the inviscid downstream value but it rose rapidly past the inviscid shock location. However, the surface pressure did not reach the downstream inviscid value and reasons were proposed for this anomalous behavior compared to strongly separated, supersonic interactions. The second class of interactions involved weak shocks impinging near small expansion corners. As a prelude to studying this interaction, a hypersonic similarity parameter was identified for the pure, expansion corner flow. The expansion corner severely damped out surface pressure fluctuations. When a shock impinged upstream of the corner, no significant changes to the surface pressure were found as compared to the case when the shock impinged on a flat plate. But, when the shock impinged downstream of the corner, a close coupling existed between the two wave systems, unlike the supersonic case. This close coupling modified the upstream influence. Regardless of whether the shock impinged ahead or behind the corner, the downstream region was affected by the close coupling between the shock and the expansion. Not only was the mean pressure distribution modified but the un...
Author : Chen-Chih Sun
Publisher :
ISBN 13 :
Total Pages : 916 pages
Book Rating : 4.:/5 (31 download)
Download or read book An experimental investigation of shock wave-turbulent boundary layer interactions with and without boundary layer suction written by Chen-Chih Sun and published by . This book was released on 1977 with total page 916 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James M. Kendall
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (976 download)
Download or read book Experimental Investigation of Leading Edge Shock Wave-boundary Layer Interaction at Hypersonic Speeds written by James M. Kendall and published by . This book was released on 1956 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Konstantinos Kontis
Publisher : Springer
ISBN 13 : 3319731807
Total Pages : 408 pages
Book Rating : 4.3/5 (197 download)
Download or read book Shock Wave Interactions written by Konstantinos Kontis and published by Springer. This book was released on 2018-03-28 with total page 408 pages. Available in PDF, EPUB and Kindle. Book excerpt: This edited monograph contains the proceedings of the International Shock Interaction Symposium, which emerged as an heir to both the Mach Reflection and Shock Vortex Interaction Symposia. These scientific biannual meetings provide an ideal platform to expose new developments and discuss recent challenges in the field of shock wave interaction phenomena. The goal of the symposia is to offer a forum for international interaction between young and established scientists in the field of shock and blast wave interaction phenomena. The target audience of this book comprises primarily researchers and experts in the field of shock waves, but the book may also be beneficial for young scientists and graduate students alike.
Author : Holger Babinsky
Publisher : Cambridge University Press
ISBN 13 : 1139498649
Total Pages : 481 pages
Book Rating : 4.1/5 (394 download)
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 : John Warren Welch
Publisher :
ISBN 13 :
Total Pages : 348 pages
Book Rating : 4.:/5 (161 download)
Download or read book An Experimental Investigation of a Three-dimensional Shock Wave-turbulent Boundary Layer Interaction in Supersonic Flow written by John Warren Welch and published by . This book was released on 1987 with total page 348 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James Madison Kendall
Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.:/5 (437 download)
Download or read book An Experimental Investigation of Leading Edge Shock Wave-boundary Layer Interaction at Hypersonic Speeds written by James Madison Kendall and published by . This book was released on 1956 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Michael S. Holden
Publisher :
ISBN 13 :
Total Pages : 96 pages
Book Rating : 4.3/5 (91 download)
Download or read book A Study of Flow Separation in Regions of Shock Wave-boundary Layer Interaction in Hypersonic Flow written by Michael S. Holden and published by . This book was released on 1975 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes a theoretical and experimental investigation of the properties of attached and separated regions of shock wave-laminar boundary layer interacting in the strong interaction regime. The flow is studied over a flat plate-wedge compression surface in the high Mach number, low Reynolds number regime where the interaction between the viscous and inviscid regions over the basic flat plate is strong and of fundamental importance to the problem. The theoretical analysis treats the development of the viscous layer and its interaction with the external inviscid stream, using an integral representation for the boundary layer equations. A complementary experimental study investigated the flow over a flat plate-wedge compression surface for a range of free-stream Reynolds number and Mach number conditions in the strong interaction regime.
Author : Anne-Marie Schreyer
Publisher :
ISBN 13 : 9783843912662
Total Pages : 0 pages
Book Rating : 4.9/5 (126 download)
Download or read book Experimental investigations of supersonic and hypersonic shock wave/turbulent boundary layer interactions written by Anne-Marie Schreyer and published by . This book was released on 2012 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.:/5 (317 download)
Download or read book An Experimental Documentation of a Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flow: With and Without Separation written by and published by . This book was released on 1975 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
