Surface and Flow Field Measurements in a Symmetric Crossing Shock Wave/turbulent Boundary-layer Interaction
Author: D. O. Davis
Publisher:
Published: 1992
Total Pages: 24
ISBN-13:
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Author: D. O. Davis
Publisher:
Published: 1992
Total Pages: 24
ISBN-13:
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Publisher:
Published: 1994
Total Pages: 492
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: 456
ISBN-13:
DOWNLOAD EBOOKLists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: Hyun D. Kim
Publisher:
Published: 1996
Total Pages: 14
ISBN-13:
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Publisher:
Published: 1994
Total Pages: 1284
ISBN-13:
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Publisher:
Published: 1948
Total Pages: 400
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DOWNLOAD EBOOKAuthor: American Institute of Aeronautics and Astronautics
Publisher:
Published: 2004
Total Pages: 954
ISBN-13:
DOWNLOAD EBOOKAuthor: Tianshu Liu
Publisher: Springer Science & Business Media
Published: 2006-01-06
Total Pages: 331
ISBN-13: 3540266445
DOWNLOAD EBOOKLuminescent molecule sensors, called pressure-sensitive paint (PSP) and temperature-sensitive paint (TSP), measure factors essential for understanding the aerodynamic performance and heat transfer characteristics of flight vehicles. They provide a powerful tool for experimental aerodynamicists to obtain a deeper understanding of the rich physical phenomena in complex flows around a flight vehicle. This book helps the reader to understand the physics and chemistry and the capabilities of PSP and TSP. It provides an overview of the wide scope of applications and explains the system requirements for using these sensors. The book also includes an extensive table of properties of PTP and TSP. As such, it is a thorough and up-to-date coverage of the underlying physics and applications of luminescent molecules designed for global pressure and temperature mapping
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Published: 1994
Total Pages:
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