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Kunyuan Zhang
Hypersonic Curved Compression Inlet and Its Inverse Design
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4196314Hypersonic Curved Compression Inlet and Its Inverse Designhttps://www.gandhi.com.mx/hypersonic-curved-compression-inlet-and-its-inverse-design-9789811507274/phttps://gandhi.vtexassets.com/arquivos/ids/3593030/d8479091-5cab-45c5-8110-ef8aa0392f3f.jpg?v=63838559842213000040234470MXNSpringer Nature SingaporeInStock/Ebooks/<p>This book presents systematic research results on curved shock wave-curved compression surface applied to the compression surface design of supersonichypersonic inlet, which is a brand new inlet design. The concept of supersonic inlet curved compression discussed originated from the authors 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.</p>...4132884Hypersonic Curved Compression Inlet and Its Inverse Design40234470https://www.gandhi.com.mx/hypersonic-curved-compression-inlet-and-its-inverse-design-9789811507274/phttps://gandhi.vtexassets.com/arquivos/ids/3593030/d8479091-5cab-45c5-8110-ef8aa0392f3f.jpg?v=638385598422130000InStockMXN99999DIEbook20209789811507274_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_<p>This book presents systematic research results on curved shock wave-curved compression surface applied to the compression surface design of supersonichypersonic inlet, which is a brand new inlet design. The concept of supersonic inlet curved compression discussed originated from the authors 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.</p>9789811507274_Springer Singaporelibro_electonico_58f9f289-b9f1-3110-91b4-6ede96beb224_9789811507274;9789811507274_9789811507274Kunyuan ZhangInglésMéxico2020-01-22T00:00:00+00:00Springer Singapore