國立高雄大學圖資館 |

Language: English

Back

Transition location effect on shock ...

Doerffer, Piotr.

Transition location effect on shock wave boundary layer interactionexperimental and numerical findings from the TFAST Project /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Transition location effect on shock wave boundary layer interactionedited by Piotr Doerffer ... [et al.].
Reminder of title:	experimental and numerical findings from the TFAST Project /
other author:	Doerffer, Piotr.
Published:	Cham :Springer International Publishing :2021.
Description:	viii, 540 p. :ill., digital ;24 cm.
Contained By:	Springer Nature eBook
Subject:	Boundary layerMathematics.
Online resource:	https://doi.org/10.1007/978-3-030-47461-4
ISBN:	9783030474614$q(electronic bk.)

Transition location effect on shock wave boundary layer interactionexperimental and numerical findings from the TFAST Project /
Transition location effect on shock wave boundary layer interactionexperimental and numerical findings from the TFAST Project /[electronic resource] :edited by Piotr Doerffer ... [et al.]. - Cham :Springer International Publishing :2021. - viii, 540 p. :ill., digital ;24 cm. - Notes on numerical fluid mechanics and multidisciplinary design,v.1441612-2909 ;. - Notes on numerical fluid mechanics and multidisciplinary design ;118..

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.

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.

ISBN: 9783030474614$q(electronic bk.)

Standard No.: 10.1007/978-3-030-47461-4doiSubjects--Topical Terms:

887041
Boundary layer
--Mathematics.

LC Class. No.: QA913 / .T73 2021

Dewey Class. No.: 532.05

Transition location effect on shock wave boundary layer interactionexperimental and numerical findings from the TFAST Project /
LDR:02821nmm a2200337 a 4500 001 594911
003 DE-He213
005 20200730164123.0
006 m d
007 cr nn 008maaau
008 211005s2021 sz s 0 eng d
020 $a 9783030474614$q(electronic bk.)
020 $a 9783030474607$q(paper)
024 7 $a 10.1007/978-3-030-47461-4 $2 doi
035 $a 978-3-030-47461-4
040 $a GP $c GP
041 0 $a eng
050 4 $a QA913 $b .T73 2021
072 7 $a TGMF $2 bicssc
072 7 $a TEC009070 $2 bisacsh
072 7 $a TGMF $2 thema
082 0 4 $a 532.05 $2 23
090 $a QA913 $b .T772 2021
245 0 0 $a Transition location effect on shock wave boundary layer interaction $h [electronic resource] : $b experimental and numerical findings from the TFAST Project / $c edited by Piotr Doerffer ... [et al.].
260 $a Cham : $b Springer International Publishing : $b Imprint: Springer, $c 2021.
300 $a viii, 540 p. : $b ill., digital ; $c 24 cm.
490 1 $a Notes on numerical fluid mechanics and multidisciplinary design, $x 1612-2909 ; $v v.144
505 0 $a 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 $a 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.
650 0 $a Boundary layer $x Mathematics. $3 887041
650 0 $a Shock waves. $3 278840
650 1 4 $a Engineering Fluid Dynamics. $3 273893
650 2 4 $a Fluid- and Aerodynamics. $3 376797
650 2 4 $a Engine Technology. $3 601259
650 2 4 $a Engineering Thermodynamics, Heat and Mass Transfer. $3 338996
700 1 $a Doerffer, Piotr. $3 492275
710 2 $a SpringerLink (Online service) $3 273601
773 0 $t Springer Nature eBook
830 0 $a Notes on numerical fluid mechanics and multidisciplinary design ; $v 118. $3 558145
856 4 0 $u https://doi.org/10.1007/978-3-030-47461-4
950 $a Engineering (SpringerNature-11647)