Téléchargez le livre : Hypersonic Curved Compression Inlet and Its Inverse Design

Hypersonic Curved Compression Inlet and Its Inverse Design

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Éditeur :

Springer


Collection :

Advanced Topics in Science and Technology in China

Paru le : 2020-01-22

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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.
Pages
332 pages
Collection
Advanced Topics in Science and Technology in China
Parution
2020-01-22
Marque
Springer
EAN papier
9789811507267
EAN PDF
9789811507274
Informations sur l'ebook
Nombre pages copiables
3
Nombre pages imprimables
33
Taille du fichier
22528 Ko
Prix
220,49 €
EAN EPUB
9789811507274
Informations sur l'ebook
Nombre pages copiables
3
Nombre pages imprimables
33
Taille du fichier
81091 Ko
Prix
220,49 €

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