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A Computational Investigation Of The Incipient Separation Of A Hypersonic Turbulent Boundary Layer
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Book Synopsis A Computational Investigation of the Incipient Separation of a Hypersonic Turbulent Boundary Layer by : J. A. Edwards
Download or read book A Computational Investigation of the Incipient Separation of a Hypersonic Turbulent Boundary Layer written by J. A. Edwards and published by . This book was released on 1997 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Pressure Rise Required for Incipient Separation of Turbulent Boundary Layers in 2-dimensional Supersonic Flow [with List of References] by :
Download or read book Experimental Investigation of Pressure Rise Required for Incipient Separation of Turbulent Boundary Layers in 2-dimensional Supersonic Flow [with List of References] written by and published by . This book was released on 1959 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.
Book Synopsis Experimental Investigation of the Pressure Rise Required for the Incipient Separation of Turbulent Boundary Layers in Two-dimensional Supersonic Flow by : Donald M. Kuehn
Download or read book Experimental Investigation of the Pressure Rise Required for the Incipient Separation of Turbulent Boundary Layers in Two-dimensional Supersonic Flow written by Donald M. Kuehn and published by . This book was released on 1959 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic-turbulent Boundary-layer Separation Over a Cone-cylinder-flare Configuration by : Arnold Polak
Download or read book Hypersonic-turbulent Boundary-layer Separation Over a Cone-cylinder-flare Configuration written by Arnold Polak and published by . This book was released on 1969 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results of a study of hypersonic-turbulent boundary-layer separation over axisymmetric bodies are presented. Pressure, heat-transfer and flow visualization data were obtained for a cone-cylinder-flare configuration. The experimental data were correlated with a theoretical prediction. (Author).
Book Synopsis Numerical Investigation of Compressible Turbulent Boundary Layers by : Muhammad Farrukh Shahab
Download or read book Numerical Investigation of Compressible Turbulent Boundary Layers written by Muhammad Farrukh Shahab and published by LAP Lambert Academic Publishing. This book was released on 2012-02 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt: As a prerequisite for relevant model development and improvement of design methodologies for supersonic vehicles, this study aims at investigating the influence of wall heat-transfer and shock interaction on the turbulence structure of supersonic boundary layers. Incipient separation conditions and two different wall thermal boundary conditions (adiabatic and cold) are considered. The analysis focuses on the evolution of mean and turbulent flow properties along the interaction region and in the relaxation region downstream of the shock-system. The strong influence of the mean pressure gradient is quantified through the analysis of mean flow profiles and boundary layer integral parameters. The anisotropic amplification of turbulent quantities through the interaction region is characterized and the turbulent events associated with the modification of the turbulence structure of the perturbed boundary layer are identified. The mean and turbulent thermal fields are shown to be strongly modified by the wall cooling which significantly dampens more particularly the turbulent thermal quantities levels across the boundary layer.
Book Synopsis Incipient Separation of a Turbulent Boundary Layer at High Reynolds Number in Two- Dimensional Supersonic Flow Over a Compression Corner by :
Download or read book Incipient Separation of a Turbulent Boundary Layer at High Reynolds Number in Two- Dimensional Supersonic Flow Over a Compression Corner written by and published by . This book was released on 1969 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Incipient Separation of a Supersonic, Turbulent Boundary Layer Including Effects of Heat Transfer by : John Carrol Frishett
Download or read book Incipient Separation of a Supersonic, Turbulent Boundary Layer Including Effects of Heat Transfer written by John Carrol Frishett and published by . This book was released on 1971 with total page 272 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Aeronautical Journal written by and published by . This book was released on 2001 with total page 732 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Computational Study of Hypersonic Boundary Layer Stability on a Blunt Nose Flared Cone Model by : Ndaona Chokani
Download or read book A Computational Study of Hypersonic Boundary Layer Stability on a Blunt Nose Flared Cone Model written by Ndaona Chokani and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Incipient Separation of a Supersonic Turbulent Boundary Layer at Moderate to High Reynolds Numbers by : Gary S. Settles
Download or read book Incipient Separation of a Supersonic Turbulent Boundary Layer at Moderate to High Reynolds Numbers written by Gary S. Settles and published by . This book was released on 1975 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Supersonic Turbulent Boundary-layer Separation on a Compression Ramp by an Integral Method by :
Download or read book Investigation of Supersonic Turbulent Boundary-layer Separation on a Compression Ramp by an Integral Method written by and published by . This book was released on 1977 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Incipient Separation and Similitude Properties of Swept Shock Turbulent Boundary Layer Interactions by : George R. Inger
Download or read book Incipient Separation and Similitude Properties of Swept Shock Turbulent Boundary Layer Interactions written by George R. Inger and published by . This book was released on 1986 with total page 32 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 1999 with total page 1044 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flow Separation in Shock Wave Boundary Layer Interactions at Hypersonic Speeds by : Awatef Hamed
Download or read book Flow Separation in Shock Wave Boundary Layer Interactions at Hypersonic Speeds written by Awatef Hamed and published by . This book was released on 1990 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Study on High Subsonic Turbulent Flow Incipient Separation and Hole/boundary Layer Interaction by : Hideki Kuwano
Download or read book Study on High Subsonic Turbulent Flow Incipient Separation and Hole/boundary Layer Interaction written by Hideki Kuwano and published by . This book was released on 1976 with total page 98 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 1992 with total page 324 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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