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[null,"1.","Record Nr.",null,"UNINA9910897162903321"]
[null,null,"Titolo",null,"New York herald tribune"]
[null,null,"Pubbl/distr/stampa",null,"New York, N.Y., : Toby Mamis, 196-"]
[null,null,"Descrizione fisica",null,"1 online resource"]
[null,null,"Soggetti",null,"Student publications - New York (State) - New York"]
[{"$nulls":4},"Underground press publications - New York (State) - New York"]
[{"$nulls":4},"New York (N.Y.) Social conditions Newspapers"]
[{"$nulls":4},"New York County (N.Y.) Newspapers"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Periodico"]
[null,null,null,"Note generali","Published by: High School Student Union."]
[null,"2.","Record Nr.",null,"UNINA9910299711203321"]
[null,null,"Autore",null,"Hirschel Ernst Heinrich"]
[null,null,"Titolo",null,"Three-dimensional attached viscous flow : basic principles and theoretical foundations / / by Ernst Heinrich Hirschel, Jean Cousteix, Wilhelm Kordulla"]
[null,null,"Pubbl/distr/stampa",null,"Berlin, Heidelberg : , : Springer Berlin Heidelberg : , : Imprint : Springer, , 2014"]
[null,null,"ISBN",null,"3-642-41378-1"]
[null,null,"Edizione",null,"[1st ed. 2014.]"]
[null,null,"Descrizione fisica",null,"1 online resource (396 p.)"]
[null,null,"Disciplina",null,"532"]
[{"$nulls":4},"533.62"]
[{"$nulls":4},"620"]
[{"$nulls":4},"620.1064"]
[null,null,"Soggetti",null,"Aerospace engineering"]
[{"$nulls":4},"Astronautics"]
[{"$nulls":4},"Fluid mechanics"]
[{"$nulls":4},"Fluids"]
[{"$nulls":4},"Thermodynamics"]
[{"$nulls":4},"Heat engineering"]
[{"$nulls":4},"Heat - Transmission"]
[{"$nulls":4},"Mass transfer"]
[{"$nulls":4},"Aerospace Technology and Astronautics"]
[{"$nulls":4},"Engineering Fluid Dynamics"]
[{"$nulls":4},"Fluid- and Aerodynamics"]
[{"$nulls":4},"Engineering Thermodynamics, Heat and Mass Transfer"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","Description based upon print version of record."]
[null,null,null,"Nota di bibliografia","Includes bibliographical references and index."]
[null,null,"Nota di contenuto",null,"Introduction -- Properties of Three-Dimensional Attached Viscous Flow -- Equations of Motion -- Boundary-Layer Equations for Three-Dimensional Flow -- Boundary-Layer Integral Parameters -- Viscous Flow and Inviscid Flow Connections and Interactions -- Topology of Skin-Friction Fields -- Quasi-One-Dimensional and Quasi-Two-Dimensional Flows -- Laminar-Turbulent Transition and Turbulence -- Illustrating Examples -- Solutions of the Problems."]
[null,null,null,"Sommario/riassunto","Viscous flow is usually treated in the frame of boundary-layer theory "]
[{"$nulls":4},"and as a two-dimensional flow. At best, books on boundary layers provide the describing equations for three-dimensional boundary layers, and solutions only for certain special cases. This book presents the basic principles and theoretical foundations of three-dimensional attached viscous flows as they apply to aircraft of all kinds. Though the primary flight speed range is that of civil air transport vehicles, flows past other flying vehicles up to hypersonic speeds are also considered. Emphasis is put on general three-dimensional attached viscous flows and not on three-dimensional boundary layers, as this wider scope is necessary in view of the theoretical and practical problems that have to be overcome in practice. The specific topics covered include weak, strong, and global interaction; the locality principle; properties of three-dimensional viscous flows; thermal surface effects; characteristic properties; wall compatibility conditions; connections between inviscid and viscous flows; flow topology; quasi-one- and two-dimensional flows; laminar-turbulent transition; and turbulence. Detailed discussions of examples illustrate these topics and the relevant phenomena encountered in three-dimensional viscous flows. The full governing equations, reference-temperature relations for qualitative considerations and estimations of flow properties, and coordinates for fuselages and wings are also provided. Sample problems with solutions allow readers to test their understanding. ."]