Experimental Investigation of Supersonic Boundary-layer Flows with Pressure Gradients
Author: S. Sivasegaram
Publisher:
Published: 1969
Total Pages:
ISBN-13: 9780114704582
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Author: S. Sivasegaram
Publisher:
Published: 1969
Total Pages:
ISBN-13: 9780114704582
DOWNLOAD EBOOKAuthor: Markus Raffel
Publisher: Springer Science & Business Media
Published: 2007-08-09
Total Pages: 460
ISBN-13: 3540723072
DOWNLOAD EBOOKThis immensely practical guide to PIV provides a condensed, yet exhaustive guide to most of the information needed for experiments employing the technique. This second edition has updated chapters on the principles and extra information on microscopic, high-speed and three component measurements as well as a description of advanced evaluation techniques. What’s more, the huge increase in the range of possible applications has been taken into account as the chapter describing these applications of the PIV technique has been expanded.
Author: United States. Wright Air Development Division
Publisher:
Published: 1961
Total Pages: 1246
ISBN-13:
DOWNLOAD EBOOKAuthor: Holger Babinsky
Publisher: Cambridge University Press
Published: 2011-09-12
Total Pages: 481
ISBN-13: 1139498649
DOWNLOAD EBOOKShock 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.
Author:
Publisher:
Published: 1995
Total Pages: 704
ISBN-13:
DOWNLOAD EBOOKAuthor: F. K. Moore
Publisher: Princeton University Press
Published: 2015-12-08
Total Pages: 892
ISBN-13: 1400875374
DOWNLOAD EBOOKVolume IV of the High Speed Aerodynamics and Jet Propulsion series. Contents of this volume include: Introduction, by F.K. Moore; Laminar Flow Theory, by P.A. Lagerstrom; Three-Dimensional Laminar Boundary Layers, by A. Mager; Theory of Time-Dependent Laminar Flows, by Nicholas Rott; Hypersonic Boundary Layer Theory, by F.K. Moore; Laminar Flows with Body Forces, by Simon Ostrach; Stability of Laminar Flows, by S.F. Shen. Originally published in 1964. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author: Jim J. Jones
Publisher:
Published: 1957
Total Pages: 716
ISBN-13:
DOWNLOAD EBOOKAn experimental investigation has been made of the attenuation of strong shock waves in air in a shock tube. Time-history measurements were made of the static pressure at several stations in the wall of the tube. The internal diameter of the tube is 3.75 inches. shock-wave-velocity data were taken for a distance along the tube of about 120 feet.
Author:
Publisher:
Published: 1974
Total Pages: 620
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Aeronautics and Space Administration
Publisher:
Published:
Total Pages: 792
ISBN-13:
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