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Shock wave-boundary layer interactions

Holger Babinsky • 2011 • Cambridge University Press

Author: Holger Babinsky
First published: 2011
Publisher: Cambridge University Press
ISBN: 9781283298261

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This volume serves as a foundational text for understanding the complex fluid dynamics involved in shock wave-boundary layer interactions. It is an essential resource for those studying the intersection of aerodynamics and high-speed flow, providing rigorous academic insight into a critical area of engineering physics.

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Shock wave-boundary layer interactions, authored by Holger Babinsky and John K. Harvey, was published by Cambridge University Press in 2011 to address the complex fluid dynamics encountered in high-speed aerospace engineering. The book emerged from a need to consolidate decades of experimental and theoretical research into a single reference, specifically focusing on the viscous interactions that occur when shock waves meet boundary layers. This phenomenon is critical to the efficiency and structural integrity of supersonic and hypersonic aircraft, as these interactions can cause significant flow separation and heat transfer issues.

The design of the volume reflects a pedagogical approach intended for graduate-level students and professional aerodynamicists. The authors synthesized fundamental physics with practical analytical methods, aiming to bridge the gap between theoretical gas dynamics and the empirical challenges faced in wind tunnel testing and flight simulation. Upon release, the work was received by the academic and engineering community as a comprehensive and authoritative text, praised for its clarity in navigating a field traditionally characterized by its intricate mathematical and physical complexities.

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