國立虎尾科技大學 |

Transition Location Effect on Shock Wave Boundary Layer Interaction = Experimental and Numerical Findings from the TFAST Project /

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Transition Location Effect on Shock Wave Boundary Layer Interaction/ edited by Piotr Doerffer, Pawel Flaszynski, Jean-Paul Dussauge, Holger Babinsky, Patrick Grothe, Anna Petersen, Flavien Billard.
其他題名:	Experimental and Numerical Findings from the TFAST Project /
其他作者:	Billard, Flavien.
面頁冊數:	VIII, 540 p. 518 illus., 424 illus. in color.online resource. :
Contained By:	Springer Nature eBook
標題:	Engineering Thermodynamics, Heat and Mass Transfer. -
電子資源:	https://doi.org/10.1007/978-3-030-47461-4
ISBN:	9783030474614

Transition Location Effect on Shock Wave Boundary Layer Interaction = Experimental 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, Pawel Flaszynski, Jean-Paul Dussauge, Holger Babinsky, Patrick Grothe, Anna Petersen, Flavien Billard. - 1st ed. 2021. - VIII, 540 p. 518 illus., 424 illus. in color.online resource. - Notes on Numerical Fluid Mechanics and Multidisciplinary Design,1441860-0824 ;. - Notes on Numerical Fluid Mechanics and Multidisciplinary Design,126.

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

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

769147
Engineering Thermodynamics, Heat and Mass Transfer.

LC Class. No.: TA357-359

Dewey Class. No.: 620.1064

Transition Location Effect on Shock Wave Boundary Layer Interaction = Experimental and Numerical Findings from the TFAST Project /
LDR:03289nam a22004095i 4500 001 1051140
003 DE-He213
005 20210815043721.0
007 cr nn 008mamaa
008 220103s2021 sz | s |||| 0|eng d
020 $a 9783030474614 $9 978-3-030-47461-4
024 7 $a 10.1007/978-3-030-47461-4 $2 doi
035 $a 978-3-030-47461-4
050 4 $a TA357-359
072 7 $a TGMF $2 bicssc
072 7 $a TEC009070 $2 bisacsh
072 7 $a TGMF $2 thema
082 0 4 $a 620.1064 $2 23
245 1 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, Pawel Flaszynski, Jean-Paul Dussauge, Holger Babinsky, Patrick Grothe, Anna Petersen, Flavien Billard.
250 $a 1st ed. 2021.
264 1 $a Cham : $b Springer International Publishing : $b Imprint: Springer, $c 2021.
300 $a VIII, 540 p. 518 illus., 424 illus. in color. $b online resource.
336 $a text $b txt $2 rdacontent
337 $a computer $b c $2 rdamedia
338 $a online resource $b cr $2 rdacarrier
347 $a text file $b PDF $2 rda
490 1 $a Notes on Numerical Fluid Mechanics and Multidisciplinary Design, $x 1860-0824 ; $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 2 4 $a Engineering Thermodynamics, Heat and Mass Transfer. $3 769147
650 2 4 $a Engine Technology. $3 881220
650 2 4 $a Fluid- and Aerodynamics. $3 768779
650 1 4 $a Engineering Fluid Dynamics. $3 670525
650 0 $a Mass transfer. $3 556853
650 0 $a Heat transfer. $3 1085480
650 0 $a Heat engineering. $3 681953
650 0 $a Thermodynamics. $3 596513
650 0 $a Machinery. $3 990113
650 0 $a Engines. $3 1253521
650 0 $a Fluids. $3 671110
650 0 $a Fluid mechanics. $3 555551
700 1 $a Billard, Flavien. $e editor. $4 edt $4 http://id.loc.gov/vocabulary/relators/edt $3 1355634
700 1 $a Petersen, Anna. $e editor. $4 edt $4 http://id.loc.gov/vocabulary/relators/edt $3 1355633
700 1 $a Grothe, Patrick. $e editor. $4 edt $4 http://id.loc.gov/vocabulary/relators/edt $3 1355632
700 1 $a Babinsky, Holger. $4 edt $4 http://id.loc.gov/vocabulary/relators/edt $3 839700
700 1 $a Dussauge, Jean-Paul. $e editor. $4 edt $4 http://id.loc.gov/vocabulary/relators/edt $3 1355631
700 1 $a Flaszynski, Pawel. $e editor. $4 edt $4 http://id.loc.gov/vocabulary/relators/edt $3 1355630
700 1 $a Doerffer, Piotr. $4 edt $4 http://id.loc.gov/vocabulary/relators/edt $3 1142553
710 2 $a SpringerLink (Online service) $3 593884
773 0 $t Springer Nature eBook
776 0 8 $i Printed edition: $z 9783030474607
776 0 8 $i Printed edition: $z 9783030474621
776 0 8 $i Printed edition: $z 9783030474638
830 0 $a Notes on Numerical Fluid Mechanics and Multidisciplinary Design, $x 1612-2909 ; $v 126 $3 1254627
856 4 0 $u https://doi.org/10.1007/978-3-030-47461-4
912 $a ZDB-2-ENG
912 $a ZDB-2-SXE
950 $a Engineering (SpringerNature-11647)
950 $a Engineering (R0) (SpringerNature-43712)