Hypersonic Curved Compression Inlet and Its Inverse Design (Hardcover, 1st ed. 2020)

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.

General

Imprint:	Springer Verlag, Singapore
Country of origin:	Singapore
Series:	Advanced Topics in Science and Technology in China, 56
Release date:	2020
First published:	2020
Authors:	Kunyuan Zhang
Dimensions:	235 x 155mm (L x W)
Format:	Hardcover
Pages:	332
Edition:	1st ed. 2020
ISBN-13:	978-981-15-0726-7
Languages:	English
Subtitles:	English
Categories:	Books > Science & Mathematics > Physics > Classical mechanics > Fluid mechanics Books > Professional & Technical > Transport technology > Aerospace & aviation technology > General Books > Professional & Technical > Mechanical engineering & materials > Materials science > Mechanics of fluids > General Promotions
LSN:	981-15-0726-0
Barcode:	9789811507267

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