Unsteady Effects of Shock Wave induced Separation

Piotr Doerffer

ISBN 10: 3662505894 / ISBN 13: 9783662505892

Published by Springer, Berlin, Springer, 2016

About this Item

Druck auf Anfrage Neuware - Printed after ordering - 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 # 9783662505892

Bibliographic Details

• Title: Unsteady Effects of Shock Wave induced Separation
• Publisher: Springer, Berlin, Springer
• Publication Date: 2016
• Language: English
• ISBN 10: 3662505894
• ISBN 13: 9783662505892
• Binding: Taschenbuch
• Condition: Neu
• Dimensions: 235W x 155H x 19D millimeters 235 millimeters width by 155 millimeters height by 19 millimeters depth
• Weight: 557 grams

About this title

Synopsis

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.

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.