Understanding high‑speed shocks: how Mach reflections change the flow math provide insight for advanced aerodynamics.
This book‑level discussion surveys different shock configurations that arise when a flow meets a boundary. It explains how a branch point and a separation line shape the pressure and velocity in each region, and it compares ordinary and Mach reflections in detail. The material is presented with analytic methods and reference to tables and figures, offering a rigorous look at how theory matches observed behavior.
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Seller: Forgotten Books, London, United Kingdom
Paperback. Condition: New. Print on Demand. This book explores a specific type of three-dimensional shock wave phenomenon known as the "Mach effect." The author offers insights into the conditions under which these configurations arise and carefully calculates the resulting pressures in a straightforward, accessible manner. These findings are placed within the broader context of shock wave research, offering a valuable resource for fluid dynamicists and engineers seeking a deeper understanding of this complex topic. This book is a reproduction of an important historical work, digitally reconstructed using state-of-the-art technology to preserve the original format. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in the book. print-on-demand item. Seller Inventory # 9781332906819_0
Quantity: Over 20 available
Seller: PBShop.store US, Wood Dale, IL, U.S.A.
PAP. Condition: New. New Book. Shipped from UK. Established seller since 2000. Seller Inventory # LW-9781332906819
Seller: PBShop.store UK, Fairford, GLOS, United Kingdom
PAP. Condition: New. New Book. Shipped from UK. Established seller since 2000. Seller Inventory # LW-9781332906819
Quantity: 15 available