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Prologue to the International Conference on Massively Separated Flows and Their Control Read chapter Read first chapter

2015 | OriginalPaper | Chapter

Some Challenging Studies on Shock Wave Boundary Layer Interactions Using Advanced Flow Diagnostics

Authors : K. Kontis, H. Zare-Behtash, E. Erdem

Published in: Instability and Control of Massively Separated Flows

Publisher: Springer International Publishing

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Abstract

Those working in the field of diagnostics continuously find new ways to visualise and quantify complicated flows in ways that were probably at some time thought to be impractical. These include either optimisation of already well-established techniques such as Schlieren with the development of higher resolution and faster cameras, or the invention of new methods by the synergy between different disciplines, such as pressure sensitive paints which bring together physics, chemistry and fluids. Ideally most of these diagnostic methods have a low parasitic profile or are completely non-intrusive. The present article paper gives a brief overview of some challenging investigations on shock boundary layer interactions using these flow diagnostic methods. A case study on axisymmetric transitional interactions at Mach 5 is also presented.

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previous chapter Investigations of Stability and Transition of a Jet in Crossflow Using DNS
next chapter Investigation of Coherent Structures and Dynamics Using POD and DMD of a Separated Airfoil Subjected to ZNMF Jet Forcing
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Metadata
Title
Some Challenging Studies on Shock Wave Boundary Layer Interactions Using Advanced Flow Diagnostics
Authors
K. Kontis
H. Zare-Behtash
E. Erdem
Copyright Year
2015
Book
Instability and Control of Massively Separated Flows

Print ISBN: 978-3-319-06259-4

Electronic ISBN: 978-3-319-06260-0

Copyright Year: 2015

DOI
https://doi.org/10.1007/978-3-319-06260-0_3

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