東華大學圖書館 |

語系: 繁體中文

說明(常見問題)

回圖書館首頁

手機版館藏查詢

登入

回首頁

切換: 標籤 | MARC模式 | ISBD

Transition location effect on shock ...

Doerffer, Piotr.

FindBook

Google Book

Amazon

博客來

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

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Transition location effect on shock wave boundary layer interaction/ edited by Piotr Doerffer ... [et al.].
其他題名:	experimental and numerical findings from the TFAST Project /
其他作者:	Doerffer, Piotr.
出版者:	Cham :Springer International Publishing : : 2021.,
面頁冊數:	viii, 540 p. :ill., digital ;24 cm.
內容註:	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.
Contained By:	Springer Nature eBook
標題:	Boundary layer - Mathematics. -
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 ... [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 ;v.144..

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:

3485904
Boundary layer
--Mathematics.

LC Class. No.: QA913 / .T73 2021

Dewey Class. No.: 532.05

Transition location effect on shock wave boundary layer interaction = experimental and numerical findings from the TFAST Project /
LDR:02821nmm a2200337 a 4500 001 2235435
003 DE-He213
005 20200730164123.0
006 m d
007 cr nn 008maaau
008 211111s2021 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 3485904
650 0 $a Shock waves. $3 661569
650 1 4 $a Engineering Fluid Dynamics. $3 891349
650 2 4 $a Fluid- and Aerodynamics. $3 1066670
650 2 4 $a Engine Technology. $3 1774726
650 2 4 $a Engineering Thermodynamics, Heat and Mass Transfer. $3 1002079
700 1 $a Doerffer, Piotr. $3 1244453
710 2 $a SpringerLink (Online service) $3 836513
773 0 $t Springer Nature eBook
830 0 $a Notes on numerical fluid mechanics and multidisciplinary design ; $v v.144. $3 3485903
856 4 0 $u https://doi.org/10.1007/978-3-030-47461-4
950 $a Engineering (SpringerNature-11647)