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010   $a981-15-0727-9
024 7 $a10.1007/978-981-15-0727-4
035   $a(CKB)4100000010119198
035   $a(DE-He213)978-981-15-0727-4
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035   $a(PPN)24284281X
035   $a(EXLCZ)994100000010119198
100   $a20200122d2020      uy             0
101 0 $aeng
135   $aurnn#|||mamaa
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aHypersonic curved compression inlet and its inverse design /$fKunyuan Zhang
205   $a1st edition 2020.
210  1$aSingapore :$cSpringer Singapore :$cImprint: Springer,$d2020.
215   $a1 online resource (XIV, 332 p.)$c391 illus., 288 illus. in color
225 1 $aAdvanced Topics in Science and Technology in China,$x1995-6819 ;$v56
311 1 $a981-15-0726-0 
327   $aIntroduction -- Calculation and Analysis Method of Two Dimensional Curved Shock Wave Curved Compression Flow Field -- Forward Design of Two Dimensional Curved Shock Wave Curved Compression Surface -- Inverse Design of Compression Inlet with Specified Exit Aerodynamic Parameters -- Inverse Design of Curved Shock Wave Compression Surface on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design of Axisymmetric Reference Flow Field on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design and Experiment of Hypersonic Curved Shock Wave Compression Inlet -- Concept of Hypersonic Adaptive Variable Geometric Curved Compression Inlet -- Features and Drag Reduction Analysis of Drag in Hypersonic Inlet -- The Development of Curved Compression and Application Prospect.
330   $aThis book presents systematic research results on curved shock wave-curved compression surface applied to the compression surface design of supersonic?hypersonic inlet, which is a brand new inlet design. The concept of supersonic inlet curved compression discussed originated from the author?s research at the Deutsches Zentrum fur Luft- und Raumfahrt (DLR SM-ES) in the early 1990s. This book introduces the research history, working characteristics, performance calculation and aerodynamic configuration design method of this compression mode in detail. It also describes method of estimating the minimum drag in inlet and drag reduction effect of curved compression and proposes a new index for evaluating unit area compression efficiency of the inlet. Further, it reviews the relevant recent research on curved compression. As such it is a valuable resource for students, researchers and scientists in the fields of hypersonic propulsion and aeronautics.
410  0$aAdvanced Topics in Science and Technology in China,$x1995-6819 ;$v56
606   $aAerodynamics, Hypersonic
606   $aCurves
606   $aFluid- and Aerodynamics$3https://scigraph.springernature.com/ontologies/product-market-codes/P21026
606   $aEngineering Fluid Dynamics$3https://scigraph.springernature.com/ontologies/product-market-codes/T15044
606   $aAerospace Technology and Astronautics$3https://scigraph.springernature.com/ontologies/product-market-codes/T17050
606   $aFluid- and Aerodynamics$3https://scigraph.springernature.com/ontologies/product-market-codes/P21026
615  0$aAerodynamics, Hypersonic.
615  0$aCurves.
615 14$aFluid- and Aerodynamics.
615 24$aEngineering Fluid Dynamics.
615 24$aAerospace Technology and Astronautics.
615 24$aFluid- and Aerodynamics.
676   $a629.132306
700   $aZhang$b Kun-Yuan$4aut$4http://id.loc.gov/vocabulary/relators/aut$01253531
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910373956303321
996   $aHypersonic curved compression inlet and its inverse design$92906344
997   $aUNINA