01125nam0 2200313 450 00003671920140903164851.020140617d--------km-y0itaa50------baengGBLady Nairne and her songsby George HendersonNew and enlarged edPaisley, LondonAlexander Gardner[s.d.]XIV, 127 p., [12] carte di tav., [1] carta di tav. ripieg.ill.18 cm.Canzoni782.42(22. ed.)Musica vocale. CanzoniHenderson,George211953ITUniversità della Basilicata - B.I.A.REICATunimarc000036719Lady Nairne and her songs102762UNIBASLETTERESTD1000120140617BAS010912STD1000120140617BAS010916TTM3020140903BAS011648BATCH0020180801BAS011239BAS01BAS01BOOKBASA1Polo Storico-UmanisticoFROSFondo RostirollaFRost/25542554D25542014061798Consultazioneall 000921103944nam 22005655 450 99641817030331620220826180137.0981-15-0727-910.1007/978-981-15-0727-4(CKB)4100000010119198(DE-He213)978-981-15-0727-4(MiAaPQ)EBC6027158(PPN)24284281X(EXLCZ)99410000001011919820200122d2020 uy 0engurnn#|||mamaatxtrdacontentcrdamediacrrdacarrierHypersonic curved compression inlet and its inverse design /Kunyuan Zhang1st edition 2020.Singapore :Springer Singapore :Imprint: Springer,2020.1 online resource (XIV, 332 p.)391 illus., 288 illus. in colorAdvanced Topics in Science and Technology in China,1995-6819 ;56981-15-0726-0 Introduction -- 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.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.Advanced Topics in Science and Technology in China,1995-6819 ;56Aerodynamics, HypersonicCurvesFluid- and Aerodynamicshttps://scigraph.springernature.com/ontologies/product-market-codes/P21026Engineering Fluid Dynamicshttps://scigraph.springernature.com/ontologies/product-market-codes/T15044Aerospace Technology and Astronauticshttps://scigraph.springernature.com/ontologies/product-market-codes/T17050Fluid- and Aerodynamicshttps://scigraph.springernature.com/ontologies/product-market-codes/P21026Aerodynamics, Hypersonic.Curves.Fluid- and Aerodynamics.Engineering Fluid Dynamics.Aerospace Technology and Astronautics.Fluid- and Aerodynamics.629.132306Zhang Kun-Yuanauthttp://id.loc.gov/vocabulary/relators/aut1253531MiAaPQMiAaPQMiAaPQBOOK996418170303316Hypersonic curved compression inlet and its inverse design2906344UNISA