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Advanced Topics in Science and Technology in China

Hypersonic Curved Compression Inlet and Its Inverse Design

Authors: Zhang, Kunyuan

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  • Introduces curved shock wave-curved compression surface applied to the compression surface design of supersonic velocity–hypersonic inlet
  • Provides results that can be adopted in the aerodynamic design of hypersonic airbreathing engines
  • Proposes aerodynamic configuration of inlet with excellent performance
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書籍の購入

イーブック ¥16,847
価格の適用国: Japan (日本円価格は個人のお客様のみ有効) (小計)
  • 予定日: January 22, 2020
  • ISBN 978-981-15-0727-4
  • ウォーターマーク付、 DRMフリー
  • ファイル形式: PDF, EPUB
  • どの電子書籍リーダーからでもすぐにお読みいただけます。
ハードカバー ¥21,059
価格の適用国: Japan (日本円価格は個人のお客様のみ有効) (小計)
  • 予定日: January 23, 2020
  • ISBN 978-981-15-0726-7
  • 個人のお客様には、世界中どこでも配送料無料でお届けします。
この書籍について

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.


著者について

Prof. Kunyuan Zhang is a Professor at the College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, China. He received his B.S. and M.S. degrees in Power Engineering from Nanjing Aeronautical Institute (now Nanjing University of Aeronautics and Astronautics) in 1965 and 1981, respectively, and he has been teaching at the same university since 1986. His research fields include hypersonic propulsion technology and internal flow dynamics.

Table of contents (10 chapters)

Table of contents (10 chapters)

書籍の購入

イーブック ¥16,847
価格の適用国: Japan (日本円価格は個人のお客様のみ有効) (小計)
  • 予定日: January 22, 2020
  • ISBN 978-981-15-0727-4
  • ウォーターマーク付、 DRMフリー
  • ファイル形式: PDF, EPUB
  • どの電子書籍リーダーからでもすぐにお読みいただけます。
ハードカバー ¥21,059
価格の適用国: Japan (日本円価格は個人のお客様のみ有効) (小計)
  • 予定日: January 23, 2020
  • ISBN 978-981-15-0726-7
  • 個人のお客様には、世界中どこでも配送料無料でお届けします。
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書誌情報

Bibliographic Information
Book Title
Hypersonic Curved Compression Inlet and Its Inverse Design
Authors
Series Title
Advanced Topics in Science and Technology in China
Series Volume
56
Copyright
2020
Publisher
Springer Singapore
Copyright Holder
Zhejiang University Press and Springer Nature Singapore Pte Ltd.
イーブック ISBN
978-981-15-0727-4
DOI
10.1007/978-981-15-0727-4
ハードカバー ISBN
978-981-15-0726-7
Series ISSN
1995-6819
Edition Number
1
Number of Pages
XIV, 332
Number of Illustrations
103 b/w illustrations, 288 illustrations in colour
Topics