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OverviewA 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. Full Product DetailsAuthor: Alexander J. Smits , Jean-Paul DussaugePublisher: Springer-Verlag New York Inc. Imprint: Springer-Verlag New York Inc. Edition: 2nd ed. 2006 Dimensions: Width: 15.50cm , Height: 2.30cm , Length: 23.50cm Weight: 1.710kg ISBN: 9780387261409ISBN 10: 0387261400 Pages: 410 Publication Date: 20 October 2005 Audience: College/higher education , Professional and scholarly , Undergraduate , Postgraduate, Research & Scholarly Format: Hardback Publisher's Status: Active Availability: In Print  This item will be ordered in for you from one of our suppliers. Upon receipt, we will promptly dispatch it out to you. For in store availability, please contact us. Table of ContentsEquations of Motion.- Equations for Turbulent Flow.- Fundamental Concepts.- Morkovin’s hypothesis.- Mixing Layers.- Boundary Layer Mean-Flow Behavior.- Boundary Layer Turbulence Behavior.- Perturbed Boundary Layers.- Shock Wave-Boundary Layer Interactions.ReviewsAuthor InformationTab Content 6Author Website:Countries AvailableAll regions |
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