Shock Wave/Boundary Layer Interaction (SBLI) is a fundamental
phenomenon in gasdynamics and frequently a defining feature in high
speed aerodynamic flowfields. The interactions can be found in
practical situations, ranging from transonic aircraft wings to
hypersonic vehicles and engines. SBLI's have the potential to pose
serious problems and is thus a critical issue for aerospace
applications. This is the first book devoted solely to a
comprehensive, state of the art explanation of the phenomenon with
coverage of all flow regimes where SBLI's occur. The book includes
contributions from leading international experts who share their
insight into SBLI physics and the impact of these interactions on
practical flow situations. This book is aimed at practitioners and
graduate students in aerodynamics who wish to familiarise
themselves with all aspects of SBLI flows. It is a valuable
resource for the specialist because it gathers experimental,
computational and theoretical knowledge in one place.
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