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.
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