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Unsteady Effects of Shock Wave Induced Separation [recurso electrónico] / by Piotr Doerffer, Charles Hirsch, Jean-Paul Dussauge, Holger Babinsky, George N. Barakos.

Por: Doerffer, Piotr [author.]Colaborador(es): Hirsch, Charles [author.] | Dussauge, Jean-Paul [author.] | Babinsky, Holger [author.] | Barakos, George N [author.] | SpringerLink (Online service)Tipo de material: Texto

TextoSeries Notes on Numerical Fluid Mechanics and Multidisciplinary Design ; 114Editor: Berlin, Heidelberg : Springer Berlin Heidelberg, 2011Descripción: 336p. 348 illus. online resourceTipo de contenido: text Tipo de medio: computer Tipo de portador: online resourceISBN: 9783642030048Tema(s): Engineering | Vibration | Engineering | Vibration, Dynamical Systems, Control | Classical Continuum PhysicsFormatos físicos adicionales: Printed edition:: Sin títuloClasificación CDD: 620 Clasificación LoC:TA355TA352-356Recursos en línea: Libro electrónico Texto

Contenidos:

Part I Transonic interactions -- Part II Nozzle flows -- Part III Shock reflection -- Part IV Summary by Work Packages.-.

En: Springer eBooksResumen: This volume contains description of experimental and numerical results obtained in the UFAST project. The goal of the project was to generate experiment data bank providing unsteady characteristics of the shock boundary layer interaction. This new data bank should be useful for better understanding of the physical phenomena involved. The experiments concerned basic reference cases and the cases with application of flow control devices. The devices were freely chosen by research groups, depending on their experience. Obtained new data bank was used for the comparison with available simulation techniques, starting from RANS, through URANS and LES. Significant effort was also concentrated on hybrid RANS-LES methods.

Existencias ( 1 )
Notas de título ( 3 )

Existencias
Tipo de ítem	Biblioteca actual	Colección	Signatura	Copia número	Estado	Fecha de vencimiento	Código de barras
Libro Electrónico	Biblioteca Electrónica	Colección de Libros Electrónicos	TA355 (Browse shelf(Abre debajo))	1	No para préstamo		373494-2001

Part I Transonic interactions -- Part II Nozzle flows -- Part III Shock reflection -- Part IV Summary by Work Packages.-.

This volume contains description of experimental and numerical results obtained in the UFAST project. The goal of the project was to generate experiment data bank providing unsteady characteristics of the shock boundary layer interaction. This new data bank should be useful for better understanding of the physical phenomena involved. The experiments concerned basic reference cases and the cases with application of flow control devices. The devices were freely chosen by research groups, depending on their experience. Obtained new data bank was used for the comparison with available simulation techniques, starting from RANS, through URANS and LES. Significant effort was also concentrated on hybrid RANS-LES methods.