Kunyuan Zhang

(Author)

Hypersonic Curved Compression Inlet and Its Inverse Design (2020)Hardcover - 2020, 23 January 2020

Hypersonic Curved Compression Inlet and Its Inverse Design (2020)
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Part of Series
Advanced Topics in Science and Technology in China
Print Length
332 pages
Language
English
Publisher
Springer
Date Published
23 Jan 2020
ISBN-10
9811507260
ISBN-13
9789811507267

Description

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 author's research at the Deutsches Zentrum fur Luft- und Raumfahrt (DLR SM-ES) in the early 1990s. This book introduces the research history, working characteristics, performance calculation and aerodynamic configuration design method of this compression mode in detail. It also describes method of estimating the minimum drag in inlet and drag reduction effect of curved compression and proposes a new index for evaluating unit area compression efficiency of the inlet. Further, it reviews the relevant recent research on curved compression. As such it is a valuable resource for students, researchers and scientists in the fields of hypersonic propulsion and aeronautics.

Product Details

Author:
Kunyuan Zhang
Book Edition:
2020
Book Format:
Hardcover
Country of Origin:
NL
Date Published:
23 January 2020
Dimensions:
23.39 x 15.6 x 2.06 cm
ISBN-10:
9811507260
ISBN-13:
9789811507267
Language:
English
Location:
Singapore
Pages:
332
Publisher:
Weight:
662.24 gm

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