Thermodynamics: An Engineering Approach 8th Edition

Published by McGraw-Hill Education
ISBN 10: 0-07339-817-9
ISBN 13: 978-0-07339-817-4

Chapter 17 - Compressible Flow - Problems - Page 892: 17-77C

Answer

See explanation

Work Step by Step

When the wedge half-angle $\boldsymbol{\delta}$ is greater than the maximum deflection angle $\boldsymbol{\theta}_{\text {max }}$, the shock becomes curved and detaches from the nose of the wedge, forming what is called a detached oblique shock or a bow wave. The numerical value of the shock angle at the nose is $\beta=90^{\circ}$.
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