Flowfield Measurements in a Separated and Reattached Flat Plate Turbulent Boundary Layer
Author : William Paul Patrick
Publisher :
Page : 254 pages
File Size : 49,24 MB
Release : 1987
Category : Bubbles
ISBN :
Author : William Paul Patrick
Publisher :
Page : 254 pages
File Size : 49,24 MB
Release : 1987
Category : Bubbles
ISBN :
Author :
Publisher :
Page : 702 pages
File Size : 33,33 MB
Release : 1995
Category : Aeronautics
ISBN :
Author : Center for Turbulence Research (U.S.)
Publisher :
Page : 534 pages
File Size : 23,41 MB
Release : 2008
Category : Turbulence
ISBN :
Author : Frank T. Smith
Publisher : Springer Science & Business Media
Page : 403 pages
File Size : 31,42 MB
Release : 2012-12-06
Category : Science
ISBN : 3642830005
The IUTAM Symposium on Boundary-Layer Separation, suggested by the UK National Committee of Theoretical and Applied Mechanics and supported by the International Union of Theoretical and Applied Mechanics, was held at University College London on August 26-28, 1986. The proposed theme and scope of the Symposium were designed to help to bring about the necessary interaction between experimentalists, computationalists and theoreticians for the furthering of understanding in this challenging subject. The talks and discussions were aimed at representing the very wide range and application of separating-flow phenomena, which often substantially affect the whole of fluid dynamics at medium to large Reynolds numbers, covering in particular both laminar and turbulent flow, steady or unsteady, two- or three-dimensional, small or large-scale, incompressible or compressible, external or internal, from the experimental, computational and theoretical standpoints. It was intended that about 80 scientists would participate in the Symposium, with about 25 talks being delivered, to which poster sessions with 8 contributions were added subsequently. All the speakers and poster presenters were selected by the scientific committee, although two late replacements of speakers were required. Fruitful discussions, well led by the session chairmen, took place formally after each talk and after the poster sessions and informally on other occasions including the social events. The present proceedings of the Symposium appear to reflect much of the current state of experimental, computational and theoretical work and progress in boundary-layer separation. We hope that they provide also ideas, questions and stimulation, in addition to major recent developments.
Author : Hermann Schlichting (Deceased)
Publisher : Springer
Page : 814 pages
File Size : 11,11 MB
Release : 2016-10-04
Category : Technology & Engineering
ISBN : 366252919X
This new edition of the near-legendary textbook by Schlichting and revised by Gersten presents a comprehensive overview of boundary-layer theory and its application to all areas of fluid mechanics, with particular emphasis on the flow past bodies (e.g. aircraft aerodynamics). The new edition features an updated reference list and over 100 additional changes throughout the book, reflecting the latest advances on the subject.
Author : Ki-Hyeon Sohn
Publisher :
Page : 16 pages
File Size : 29,11 MB
Release : 1998
Category : Boundary layers
ISBN :
Author : United States. Superintendent of Documents
Publisher :
Page : 1250 pages
File Size : 32,81 MB
Release : 1979
Category : United States
ISBN :
Author :
Publisher :
Page : 568 pages
File Size : 38,35 MB
Release : 1973
Category : Mechanics, Applied
ISBN :
Author : Je-Chin Han
Publisher : Taylor & Francis
Page : 865 pages
File Size : 48,94 MB
Release : 2012-11-27
Category : Science
ISBN : 1466564903
A comprehensive reference for engineers and researchers, this second edition focuses on gas turbine heat transfer issues and their associated cooling technologies for aircraft and land-based gas turbines. It provides information on state-of-the-art cooling technologies such as advanced turbine blade film cooling and internal cooling schemes. The book also offers updated experimental methods for gas turbine heat transfer and cooling research, as well as advanced computational models for gas turbine heat transfer and cooling performance predictions. The authors provide suggestions for future research within this technology and includes 800 illustrations to help clarify concepts and instruction.
Author : Holger Babinsky
Publisher : Cambridge University Press
Page : 481 pages
File Size : 32,15 MB
Release : 2011-09-12
Category : Technology & Engineering
ISBN : 1139498649
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.