Unsteady Effects of Shock Wave induced Separation. This item is unavailable.
Language: English
Published by Springer, Berlin, Springer, 2010
- Hardcover
- New

Seller: AHA-BUCH GmbH, Einbeck, GermanyAHA-BUCH GmbH
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Condition: New
£ 398.08
Item description from seller
Neuware - 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. The experiments concerned basic-reference cases and the cases with application of flow control devices. Obtained new data bank have been used for the comparison with available simulation techniques, starting from RANS, through URANS, LES and hybrid RANS-LES methods. New understanding of flow physics as well as ability of different numerical methods in the prediction of such unsteady flow phenomena will be discussed.
Seller Inventory # 9783642030031
- Title
- Unsteady Effects of Shock Wave induced Separation
- Author
- Piotr Doerffer
- Publisher
- Springer, Berlin, Springer
- Publication year
- 2010
- Condition
- Neu
- Binding
- Buch
- Language
- English
- ISBN 10
- 3642030033
- ISBN 13
- 9783642030031
- Item weight
- 658 grams
- Dimensions
- 235x155x35 mm
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. The experiments concerned basic-reference cases and the cases with application of flow control devices. Obtained new data bank have been used for the comparison with available simulation techniques, starting from RANS, through URANS, LES and hybrid RANS-LES methods. New understanding of flow physics as well as ability of different numerical methods in the prediction of such unsteady flow phenomena will be discussed.
"Synopsis" may belong to another edition of this title.
From the Back Cover
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.
"About the title" may belong to another edition of this title.