Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Spatial And Temporal Features Of A Separated Flow Field At A Convex Wall Induced By Normal Shock Wave Turbulent Boundary Layer Interaction
Download Spatial And Temporal Features Of A Separated Flow Field At A Convex Wall Induced By Normal Shock Wave Turbulent Boundary Layer Interaction full books in PDF, epub, and Kindle. Read online Spatial And Temporal Features Of A Separated Flow Field At A Convex Wall Induced By Normal Shock Wave Turbulent Boundary Layer Interaction ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Spatial and Temporal Features of a Separated Flow Field at a Convex Wall Induced by Normal Shock Wave Turbulent Boundary Layer Interaction by : P. Doerffer
Download or read book Spatial and Temporal Features of a Separated Flow Field at a Convex Wall Induced by Normal Shock Wave Turbulent Boundary Layer Interaction written by P. Doerffer and published by . This book was released on 1990 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Physics of Separated Flows — Numerical, Experimental, and Theoretical Aspects by : Klaus Gersten
Download or read book Physics of Separated Flows — Numerical, Experimental, and Theoretical Aspects written by Klaus Gersten and published by Springer Science & Business Media. This book was released on 2013-06-29 with total page 305 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume contains 37 contributions in which the research work is summarized which has been carried out between 1984 and 1990 in the Priority Research Program "Physik abgeloster Stromungen" of the Deutsche Forschungsgemeinschaft (DFG, German Research Society). The aim of the Priority Research Program was the inten sive research of the whole range of phenomena associated with separated flows. Physi cal models as well as prediction methods had to be developed based on detailed experi mental investigations. It was in accordance with the main concept of the research program that scientists working on problems of separated flows in different technical areas of application participated in this program. The following fields have been represented in the program: aerodynamics of wings and bodies, aerodynamics of auto mobiles, turbomachinery, ship hydrodynamics, hydraulics, internal flows, heat exchan gers, bio-fluid-dynamics, aerodynamics of buildings and structures. In order to concentrate on problems common in all those areas the emphasis of the program was on basic research dealing with generic geometric configurations showing the fundamental physical phenomena of separated flows. The engagement and enthusiasm of all participating scientists are highly appreciated. The program was organized such that all researchers met once a year to report on the progress of their work. Special thanks ought to go to Prof. E. A. Muller (Gottingen), Prof. H. Oertel jun. (Braunschweig), Dr. W. Schmidt (Dornier), Dr. H. -W. Stock (Dornier) and Dr. B. Wagner (Dornier), who had the functions of referees on those annual meetings.
Download or read book AIAA 90-1440 - AIAA 90-1470 written by and published by . This book was released on 1990 with total page 390 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 1990 with total page 1068 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 1985 with total page 1346 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Surface and Flow Field Measurements in a Symmetric Crossing Shock Wave/turbulent Boundary-layer Interaction by : D. O. Davis
Download or read book Surface and Flow Field Measurements in a Symmetric Crossing Shock Wave/turbulent Boundary-layer Interaction written by D. O. Davis and published by . This book was released on 1992 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Fundamental Aspects of Shock Wave - Turbulent Boundary Interactions in Transonic Flow by : G. R. Inger
Download or read book Some Fundamental Aspects of Shock Wave - Turbulent Boundary Interactions in Transonic Flow written by G. R. Inger and published by . This book was released on 1981 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt: Transonic normal shock - turbulent boundary layer interactions can significantly influence not only the local viscous flow but also the downstream behavior of the boundary layer on aerodynamic bodies. It is therefore important that fundamentally-based analytical tools be developed for describing and scaling these interaction effects. This paper examines recent progress toward this goal, with emphasis on two aspects. (1) A basic non-asymptotic triple-deck theory of non-separating two-dimensional interactions that is applicable over a wide range of practical Reynolds numbers and boundary layer profile shapes. (2) Its applicable as a local 'interactive module' in the global transonic flow field analysis of wings, including detailed comparisons with experimental data. Also discussed is the adaptability of this theory to treat interactions involving non-adiabatic wall conditions, including the prediction of incipient separation.
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1987 with total page 338 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flowfield Analysis for Successive Oblique Shock Wave-turbulent Boundary Layer Interactions by : Chen-Chih Sun
Download or read book Flowfield Analysis for Successive Oblique Shock Wave-turbulent Boundary Layer Interactions written by Chen-Chih Sun and published by . This book was released on 1976 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Interaction of a Turbulent Boundary Layer with a Normal Shock Wave Followed by an Adverse Pressure Gradient by : W. H. Schofield
Download or read book Interaction of a Turbulent Boundary Layer with a Normal Shock Wave Followed by an Adverse Pressure Gradient written by W. H. Schofield and published by . This book was released on 1983 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental study was made of the development of a turbulent boundary layer after an interaction with a normal shock wave (strong enough to cause a local separation) in a strong adverse pressure gradient. This type of flow, which occurs in air breathing engine components (e.g. supersonic intakes, transonic compressor stages and supersonic diffusers), is poorly understood and cannot be satisfactorily predicted. The measurements, made in a closed duct, extended well downstream of the shock wave interaction. Detailed results for the flow are presented and used to support two major conclusions. It is shown that the post shock adverse pressure gradient has a large effect on boundary layer development through the interaction and downstream of it. Consequently existing results for interactions without a post shock pressure gradient should not be used as a model for practical flows which typically have strong pressure gradients applied downstream of the shock wave. The second conclusions was that the shock wave in a rectangular duct produced a pronounced stabilising effect on the downstream flow. Surface flow visualization suggests that this stabilization is achieved by streamwise vortices shed into the flow from the separated region formed by the shock wave. Implications of this result to nominally two-dimensional flow situations and to flows with weak interactions without local separations are discussed.
Author :American Institute of Aeronautics and Astronautics. Technical Information Service Publisher : ISBN 13 : Total Pages :180 pages Book Rating :4.3/5 (91 download)
Book Synopsis The Finding Guide to AIAA Meeting Papers by : American Institute of Aeronautics and Astronautics. Technical Information Service
Download or read book The Finding Guide to AIAA Meeting Papers written by American Institute of Aeronautics and Astronautics. Technical Information Service and published by . This book was released on 1990 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Behavior of a Compressible Turbulent Boundary Layer in a Shock-wave-induced Adverse Pressure Gradient by : William C. Rose
Download or read book The Behavior of a Compressible Turbulent Boundary Layer in a Shock-wave-induced Adverse Pressure Gradient written by William C. Rose and published by . This book was released on 1973 with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Evolution of the Separated Flowfield in a 3-D Shock-wave/turbulent Boundary Layer Interaction by : Datta V. Gaitonde
Download or read book Evolution of the Separated Flowfield in a 3-D Shock-wave/turbulent Boundary Layer Interaction written by Datta V. Gaitonde and published by . This book was released on 1997 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Shape of the Flow Separation Zone Induced by the Incidence of a Three-dimensional Shock Wave on a Plate with Turbulent Boundary Layer by : Yu A. Panov
Download or read book The Shape of the Flow Separation Zone Induced by the Incidence of a Three-dimensional Shock Wave on a Plate with Turbulent Boundary Layer written by Yu A. Panov and published by . This book was released on 1969 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of an experimental investigation of the structure of a separated flow on a flat plate in the region of a three-dimensional shock wave - turbulent boundary layer interaction are presented for free-stream Mach number equal to 3 and Reynolds number Re equals 1.8 x 10(superscript 7). The aim of the investigation is to clarify the general principles governing three-dimensional separated flows induced by the intersection of shock waves formed by obstacles on the body surface with the boundary layer, and to supplement the scarce data available up to now. A schematic presentation of the flow pattern is given. The relationship between the characteristic geometric dimensions of the separation zone and the intensity of the incident shock wave is studied. A comparison is made between two- and three-dimensional cases. (Author).
Book Synopsis An Analytical Study of Separated Flows Induced by Shock Wave - Boundary Layer Interaction by : M. S. Holden
Download or read book An Analytical Study of Separated Flows Induced by Shock Wave - Boundary Layer Interaction written by M. S. Holden and published by . This book was released on 1966 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Influence of Suction on Shock Wave-turbulent Boundary Layer Interactions for Two-dimensional and Axially Symmetric Flows by : William R. Seebaugh
Download or read book Influence of Suction on Shock Wave-turbulent Boundary Layer Interactions for Two-dimensional and Axially Symmetric Flows written by William R. Seebaugh and published by . This book was released on 1970 with total page 148 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.
