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

By:

Doerffer, Piotr [author.]

Contributor(s):

Series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design ; 114Publisher: Berlin, Heidelberg : Springer Berlin Heidelberg, 2011Description: 336 p. 348 illus. online resourceContent type:

text

Media type:

computer

Carrier type:

online resource

ISBN:

9783642030048

Subject(s):

Genre/Form:

Electronic books.

Additional physical formats: Printed edition:: No titleDDC classification:

620 23

LOC classification:

TA355
TA352-356

Online resources:

Click here to access online

Contents:

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

In: Springer eBooksSummary: 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.

Item type:

eBooks

Average rating: 0.0 (0 votes)

Holdings ( 0 )
Title notes ( 2 )

No physical items for this record

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.