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An Experimental Investigation Of Shock Waves And Turbulent Boundary Layer Interactions In A Supersonic Flowfield Through An Annular Duct
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Book Synopsis An Experimental Investigation of Shock Waves and Turbulent Boundary Layer Interactions in a Supersonic Flowfield Through an Annular Duct by : Richard Drexel Stockbridge
Download or read book An Experimental Investigation of Shock Waves and Turbulent Boundary Layer Interactions in a Supersonic Flowfield Through an Annular Duct written by Richard Drexel Stockbridge and published by . This book was released on 1986 with total page 212 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Shock Waves and Turbulent Boundary Layer Interactions in a Supersonic Flowfield Through an Annular Duct by : Richard Drexel Stockbridge
Download or read book An Experimental Investigation of Shock Waves and Turbulent Boundary Layer Interactions in a Supersonic Flowfield Through an Annular Duct written by Richard Drexel Stockbridge and published by . This book was released on 1986 with total page 212 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of a Three-dimensional Shock Wave-turbulent Boundary Layer Interaction in Supersonic Flow by : John Warren Welch
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:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1994 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Shock Wave and Boundary Layer Interaction Near Convex Corners in Hypersonic Flow by : Sohail Mohammed
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.
Book Synopsis An Experimental Documentation of a Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flow: With and Without Separation by :
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:
Book Synopsis Experimental investigations of supersonic and hypersonic shock wave/turbulent boundary layer interactions by : Anne-Marie Schreyer
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:
Book Synopsis Documentation of Two- and Three-dimensional Hypersonic Shock Wave/turbulent Boundary Layer Interaction Flows by : Marvin I. Kussoy
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 Synopsis Turbulent Shear Layers in Supersonic Flow by : Alexander J. Smits
Download or read book Turbulent Shear Layers in Supersonic Flow written by Alexander J. Smits and published by Springer Science & Business Media. This book was released on 2006-05-11 with total page 418 pages. Available in PDF, EPUB and Kindle. Book excerpt: A good understanding of turbulent compressible flows is essential to the design and operation of high-speed vehicles. Such flows occur, for example, in the external flow over the surfaces of supersonic aircraft, and in the internal flow through the engines. Our ability to predict the aerodynamic lift, drag, propulsion and maneuverability of high-speed vehicles is crucially dependent on our knowledge of turbulent shear layers, and our understanding of their behavior in the presence of shock waves and regions of changing pressure. Turbulent Shear Layers in Supersonic Flow provides a comprehensive introduction to the field, and helps provide a basis for future work in this area. Wherever possible we use the available experimental work, and the results from numerical simulations to illustrate and develop a physical understanding of turbulent compressible flows.
Download or read book NASA SP. written by and published by . This book was released on 1993 with total page 232 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1971 with total page 1388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aeronautical Engineering written by and published by . This book was released on 1991 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications, Cumulative Index by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications, Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1976 with total page 1408 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis International Aerospace Abstracts by :
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1995 with total page 502 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1963 with total page 1196 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Interactions Entre Ondes de Choc Et Couches Limites Dans Les Ecoulements Supersoniques Et Hypersoniques by :
Download or read book Interactions Entre Ondes de Choc Et Couches Limites Dans Les Ecoulements Supersoniques Et Hypersoniques written by and published by . This book was released on 1993 with total page 298 pages. Available in PDF, EPUB and Kindle. Book excerpt: "Shock-wave/boundary-layer interactions continue to be ubiquitous phenomena in supersonic and hypersonic aerodynamics, and their importance is often critical as, for example, for hypersonic controls and for air intakes in general. This is the reason for the continuous research efforts in this field, aiming at developing reliable methodologies for future vehicle design. Results from these programmes have been reported. The present course reviews the recent progress in this field. In particular, a large part of the course is devoted to swept interactions, both laminar and turbulent, including a discussion of the following topics: (1) The flowfield structure; (2) The scaling and similarity laws; (3) The effect of shock strength on flow features; (4) The effect of shock generator geometry for a given shock strength; (5) Experimental techniques, in particular optical techniques, for the investigation of swept interactions; and (6) Contributions of numerical simulations to the understanding of swept interactions. A limiting factor in the understanding and ability to predict shock wave/boundary-layer interactions is a good knowledge of turbulence behavior. A lecture is devoted specifically to hypersonic interactions."--DTIC.
