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

Reynolds number influences on turbul...

Priyadarshana, Paththage A.

FindBook

Google Book

Amazon

博客來

Reynolds number influences on turbulent boundary layer momentum transport.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Reynolds number influences on turbulent boundary layer momentum transport./
作者:	Priyadarshana, Paththage A.
面頁冊數:	181 p.
附註:	Source: Dissertation Abstracts International, Volume: 65-09, Section: B, page: 4794.
Contained By:	Dissertation Abstracts International65-09B.
標題:	Engineering, Mechanical. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3147373
ISBN:	0496080652

Reynolds number influences on turbulent boundary layer momentum transport.
Priyadarshana, Paththage A.

Reynolds number influences on turbulent boundary layer momentum transport. - 181 p.

Source: Dissertation Abstracts International, Volume: 65-09, Section: B, page: 4794.

Thesis (Ph.D.)--The University of Utah, 2004.

There are many engineering applications at Reynolds numbers orders of magnitude higher than existing turbulent boundary layer studies. Currently, the mechanisms for turbulent transport and the Reynolds number dependence of these mechanisms are not well understood. This dissertation presents Reynolds number influences on velocity and vorticity statistics, Reynolds shear stress, and velocity-vorticity correlations for turbulent boundary layers. Well resolved hot-wire data for this study were acquired in the atmospheric surface layer at the SLTEST facility in western Utah. It is shown that during near neutral thermal stability, the flow behaves as a canonical zero pressure gradient turbulent boundary layer, in which the Reynolds number based on momentum thickness, Rtheta, is approximately 2 x 106. The present study also provides information regarding the effects of wall roughness over a limited range of roughness.

ISBN: 0496080652Subjects--Topical Terms:

783786
Engineering, Mechanical.

Reynolds number influences on turbulent boundary layer momentum transport.
LDR:03368nmm 2200325 4500 001 1847781
005 20051108095757.5
008 130614s2004 eng d
020 $a 0496080652
035 $a (UnM)AAI3147373
035 $a AAI3147373
040 $a UnM $c UnM
100 1 $a Priyadarshana, Paththage A. $3 1935812
245 1 0 $a Reynolds number influences on turbulent boundary layer momentum transport.
300 $a 181 p.
500 $a Source: Dissertation Abstracts International, Volume: 65-09, Section: B, page: 4794.
500 $a Adviser: Joe Klewicki.
502 $a Thesis (Ph.D.)--The University of Utah, 2004.
520 $a There are many engineering applications at Reynolds numbers orders of magnitude higher than existing turbulent boundary layer studies. Currently, the mechanisms for turbulent transport and the Reynolds number dependence of these mechanisms are not well understood. This dissertation presents Reynolds number influences on velocity and vorticity statistics, Reynolds shear stress, and velocity-vorticity correlations for turbulent boundary layers. Well resolved hot-wire data for this study were acquired in the atmospheric surface layer at the SLTEST facility in western Utah. It is shown that during near neutral thermal stability, the flow behaves as a canonical zero pressure gradient turbulent boundary layer, in which the Reynolds number based on momentum thickness, Rtheta, is approximately 2 x 106. The present study also provides information regarding the effects of wall roughness over a limited range of roughness.
520 $a It is observed that with increasing Rtheta, the inner normalized streamwise intensity increases. This statistic is less sensitive to wall roughness away from the roughness sublayer. In contrast, the inner normalized wall normal intensity is less sensitive to the variation of Rtheta, and it is significantly sensitive to wall roughness. Outside the viscous sublayer, the inner normalized vorticity intensity is less sensitive to both Rtheta and roughness.
520 $a A primary observation of the Reynolds stress study is that the predominant motions underlying the Reynolds shear stress undergo a significant shift from large to intermediate scales as Rtheta becomes large, irrespective of surface roughness. Quadrant analysis shows that types of motions contributing to the Reynolds stress change significantly at comparable wall normal locations with increasing Rtheta.
520 $a The mean wall normal gradients of the Reynolds shear stress and the turbulent kinetic energy have direct connections to the transport mechanisms of the turbulent boundary layer. These gradients can be expressed in terms of velocity-vorticity correlations. In this dissertation, voz and uoz correlations are presented. Here, u and v are the streamwise and the wall normal velocities, respectively, and oz is the spanwise vorticity. It is observed that voz correlations exhibit considerable sensitivity to Rtheta as well as to wall roughness. Conversely, uoz correlations are relatively less sensitive to both Rtheta and wall roughness.
590 $a School code: 0240.
650 4 $a Engineering, Mechanical. $3 783786
650 4 $a Physics, Fluid and Plasma. $3 1018402
650 4 $a Physics, Atmospheric Science. $3 1019431
690 $a 0548
690 $a 0759
690 $a 0608
710 2 0 $a The University of Utah. $3 1017410
773 0 $t Dissertation Abstracts International $g 65-09B.
790 1 0 $a Klewicki, Joe, $e advisor
790 $a 0240
791 $a Ph.D.
792 $a 2004
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3147373