Transition Location Effect on Shock Wave Boundary Layer Interaction (Record no. 78119)

000 -LEADER
fixed length control field 04657nam a22006735i 4500
001 - CONTROL NUMBER
control field 978-3-030-47461-4
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20220801220026.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 200730s2021 sz | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9783030474614
-- 978-3-030-47461-4
082 04 - CLASSIFICATION NUMBER
Call Number 620.1064
245 10 - TITLE STATEMENT
Title Transition Location Effect on Shock Wave Boundary Layer Interaction
Sub Title Experimental and Numerical Findings from the TFAST Project /
250 ## - EDITION STATEMENT
Edition statement 1st ed. 2021.
300 ## - PHYSICAL DESCRIPTION
Number of Pages VIII, 540 p. 518 illus., 424 illus. in color.
490 1# - SERIES STATEMENT
Series statement Notes on Numerical Fluid Mechanics and Multidisciplinary Design,
505 0# - FORMATTED CONTENTS NOTE
Remark 2 Introduction – TFAST Overview -- WP-1 Reference Cases of Laminar and Turbulent Interactions -- WP-2 Basic Investigation of Transition Effect -- WP-3 Internal Flows – Compressors -- WP-4 Internal Flows – Turbine -- WP-5 External Flows – Wing -- Closing Remarks.
520 ## - SUMMARY, ETC.
Summary, etc This book presents experimental and numerical findings on reducing shock-induced separation by applying transition upstream the shock wave. The purpose is to find out how close to the shock wave the transition should be located in order to obtain favorable turbulent boundary layer interaction. The book shares findings obtained using advanced flow measurement methods and concerning e.g. the transition location, boundary layer characteristics, and the detection of shock wave configurations. It includes a number of experimental case studies and CFD simulations that offer valuable insights into the flow structure. It covers RANS/URANS methods for the experimental test section design, as well as more advanced techniques, such as LES, hybrid methods and DNS for studying the transition and shock wave interaction in detail. The experimental and numerical investigations presented here were conducted by sixteen different partners in the context of the TFAST Project. The general focus is on determining if and how it is possible to improve flow performance in comparison to laminar interaction. The book mainly addresses academics and professionals whose work involves the aerodynamics of internal and external flows, as well as experimentalists working with compressible flows. It will also be of benefit for CFD developers and users, and for students of aviation and propulsion systems alike.
700 1# - AUTHOR 2
Author 2 Doerffer, Piotr.
700 1# - AUTHOR 2
Author 2 Flaszynski, Pawel.
700 1# - AUTHOR 2
Author 2 Dussauge, Jean-Paul.
700 1# - AUTHOR 2
Author 2 Babinsky, Holger.
700 1# - AUTHOR 2
Author 2 Grothe, Patrick.
700 1# - AUTHOR 2
Author 2 Petersen, Anna.
700 1# - AUTHOR 2
Author 2 Billard, Flavien.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier https://doi.org/10.1007/978-3-030-47461-4
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Cham :
-- Springer International Publishing :
-- Imprint: Springer,
-- 2021.
336 ## -
-- text
-- txt
-- rdacontent
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-- computer
-- c
-- rdamedia
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-- online resource
-- cr
-- rdacarrier
347 ## -
-- text file
-- PDF
-- rda
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Fluid mechanics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Continuum mechanics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engines.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Thermodynamics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Heat engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Heat transfer.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Mass transfer.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering Fluid Dynamics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Continuum Mechanics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engine Technology.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering Thermodynamics, Heat and Mass Transfer.
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
-- 1860-0824 ;
912 ## -
-- ZDB-2-ENG
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-- ZDB-2-SXE

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