| 書目名稱 | Hypersonic Curved Compression Inlet and Its Inverse Design |
| 編輯 | Kunyuan Zhang |
| 視頻video | http://file.papertrans.cn/431/430684/430684.mp4 |
| 概述 | 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 |
| 叢書名稱 | Advanced Topics in Science and Technology in China |
| 圖書封面 |  |
| 描述 | .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.. |
| 出版日期 | Book 2020 |
| 關(guān)鍵詞 | hypersonic propulsion; hypersonic inlet; curved shock compression; curved compression surface; inverse d |
| 版次 | 1 |
| doi | https://doi.org/10.1007/978-981-15-0727-4 |
| isbn_softcover | 978-981-15-0729-8 |
| isbn_ebook | 978-981-15-0727-4Series ISSN 1995-6819 Series E-ISSN 1995-6827 |
| issn_series | 1995-6819 |
| copyright | Zhejiang University Press and Springer Nature Singapore Pte Ltd. 2020 |
|Archiver|手機版|小黑屋|
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