Hypersonic curved compression inlet and its inverse design /

This book presents systematic research results on curved shock wave-curved compression surface applied to the compression surface design of supersonic-hypersonic inlet, which is a brand new inlet design. The concept of supersonic inlet curved compression discussed originated from the authors researc...

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Bibliographic Details
Main Author: Zhang, Kunyuan
Format: Book
Language:English
Published: Singapore : Springer, 2020
Series:Advanced topics in science and technology in China
Subjects:

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Stanford University

Holdings details from Stanford University
Call Number: ISIL:US-CST