ENGLISH

Unsteady Effects of Shock Wave Induced Separation

By Charles Hirsch , Jean-Paul Dussauge , Piotr Doerffer , Holger Babinsky , George N. Barakos (auth.)

Book information

Publisher
Springer-Verlag Berlin Heidelberg
Year
2011
ISBN
3642030033, 9783642030031, 9783642030048
DOI
10.1007/978-3-642-03004-8
LCC
QC168.85.S45 U58 2010
Open Library ID
OL25004107M
Language
english
Format
PDF
Filesize
12 MB (12458139 bytes)
Series
Notes on Numerical Fluid Mechanics and Multidisciplinary Design 114
Edition
1
Pages
336\363
Orientation
yes
Scanned
no
Time added
2012-02-04 16:00:00
Control;Classical Continuum PhysicsDynamical SystemsVibration

Description

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.

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