國立高雄大學圖資館 |

Language: English

Back

Secondary instabilities of Gortler v...

Ren, Jie.

Secondary instabilities of Gortler vortices in high-speed boundary layersmechanisms and flow control on laminar-turbulent transition /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Secondary instabilities of Gortler vortices in high-speed boundary layersby Jie Ren.
Reminder of title:	mechanisms and flow control on laminar-turbulent transition /
Author:	Ren, Jie.
Published:	Singapore :Springer Singapore :2018.
Description:	xviii, 94 p. :ill. (some col.), digital ;24 cm.
Contained By:	Springer eBooks
Subject:	Laminar flow.
Online resource:	http://dx.doi.org/10.1007/978-981-10-6832-4
ISBN:	9789811068324$q(electronic bk.)

Secondary instabilities of Gortler vortices in high-speed boundary layersmechanisms and flow control on laminar-turbulent transition /
Ren, Jie.

Secondary instabilities of Gortler vortices in high-speed boundary layersmechanisms and flow control on laminar-turbulent transition /[electronic resource] :by Jie Ren. - Singapore :Springer Singapore :2018. - xviii, 94 p. :ill. (some col.), digital ;24 cm. - Springer theses,2190-5053. - Springer theses..

This thesis first reveals the mechanism of Gortler instabilities and then demonstrates how transitions at hypersonic flows can be effectively controlled (either promoted or suppressed) with Gortler or Klebanoff modes. It focuses on understanding and controlling flow transitions from mild laminar to fully turbulent flows at high speeds--aspects that have become crucial at the dawn of an incredible era, in which hypersonic vehicles are becoming available. Once this occurs, it will be possible to travel from Beijing to Los Angeles within just 2 hours, and we will all live in a genuinely global village--and not just virtually, but physically. Gortler instabilities have often been used to promote flow transition in hypersonic vehicles. However, how Gortler instabilities are excited and how they evolve in hypersonic flows are questions that have yet to be answered.

ISBN: 9789811068324$q(electronic bk.)

Standard No.: 10.1007/978-981-10-6832-4doiSubjects--Topical Terms:

384635
Laminar flow.

LC Class. No.: TL574.L3

Dewey Class. No.: 532.0525

Secondary instabilities of Gortler vortices in high-speed boundary layersmechanisms and flow control on laminar-turbulent transition /
LDR:01981nmm a2200337 a 4500 001 528809
003 DE-He213
005 20180620144642.0
006 m d
007 cr nn 008maaau
008 181030s2018 si s 0 eng d
020 $a 9789811068324$q(electronic bk.)
020 $a 9789811068317$q(paper)
024 7 $a 10.1007/978-981-10-6832-4 $2 doi
035 $a 978-981-10-6832-4
040 $a GP $c GP
041 0 $a eng
050 4 $a TL574.L3
072 7 $a TGMF $2 bicssc
072 7 $a TGMF1 $2 bicssc
072 7 $a TEC009070 $2 bisacsh
072 7 $a SCI085000 $2 bisacsh
082 0 4 $a 532.0525 $2 23
090 $a TL574.L3 $b R393 2018
100 1 $a Ren, Jie. $3 524294
245 1 0 $a Secondary instabilities of Gortler vortices in high-speed boundary layers $h [electronic resource] : $b mechanisms and flow control on laminar-turbulent transition / $c by Jie Ren.
260 $a Singapore : $b Springer Singapore : $b Imprint: Springer, $c 2018.
300 $a xviii, 94 p. : $b ill. (some col.), digital ; $c 24 cm.
490 1 $a Springer theses, $x 2190-5053
520 $a This thesis first reveals the mechanism of Gortler instabilities and then demonstrates how transitions at hypersonic flows can be effectively controlled (either promoted or suppressed) with Gortler or Klebanoff modes. It focuses on understanding and controlling flow transitions from mild laminar to fully turbulent flows at high speeds--aspects that have become crucial at the dawn of an incredible era, in which hypersonic vehicles are becoming available. Once this occurs, it will be possible to travel from Beijing to Los Angeles within just 2 hours, and we will all live in a genuinely global village--and not just virtually, but physically. Gortler instabilities have often been used to promote flow transition in hypersonic vehicles. However, how Gortler instabilities are excited and how they evolve in hypersonic flows are questions that have yet to be answered.
650 0 $a Laminar flow. $3 384635
650 0 $a Laminar boundary layer. $3 801424
650 1 4 $a Engineering. $3 210888
650 2 4 $a Engineering Fluid Dynamics. $3 273893
650 2 4 $a Classical Mechanics. $3 769955
650 2 4 $a Mathematical and Computational Engineering. $3 775095
710 2 $a SpringerLink (Online service) $3 273601
773 0 $t Springer eBooks
830 0 $a Springer theses. $3 557607
856 4 0 $u http://dx.doi.org/10.1007/978-981-10-6832-4
950 $a Engineering (Springer-11647)