Transition in boundary layers on a concave surface

Citation
Sh. Winoto et al., Transition in boundary layers on a concave surface, J PROPUL P, 16(4), 2000, pp. 653-660
Citations number
30
Categorie Soggetti
Aereospace Engineering
Journal title
JOURNAL OF PROPULSION AND POWER
ISSN journal
07484658 → ACNP
Volume
16
Issue
4
Year of publication
2000
Pages
653 - 660
Database
ISI
SICI code
0748-4658(200007/08)16:4<653:TIBLOA>2.0.ZU;2-1
Abstract
Transition from laminar to turbulent how has been investigated in boundary layers along a concave surface of 2.0 m radius of curvature for a freestrea m velocity range of 6.0-15.0 m/s. Velocity and turbulent intermittency meas urements were made using a single sensor hot-wire anemometer. Intermittency profiles at the so-called upwash and downwash regions were obtained at som e streamwise positions to help determine the transition starts and ends at the regions. The experimental results show that, at both upwash and downwas h regions for all of the free-stream velocities tested, the intermittency p rofiles at different transition stages exhibit similar behaviors. The diffe rence between the upwash and downwash intermittency profiles obtained at th e same streamwise locations decreases with increasing freestream velocity. For all of the freestream velocities, transition starts and ends earlier at the upwash regions than at the downwash regions. The transition lengths in the upwash regions are slightly longer than those in the downwash regions and decrease with increasing freestream velocity. The starts of transition at the upwash regions agree well with the transition prediction Goertler nu mber of 6, whereas at the ends of transition for both upwash and downwash r egions, the Goertler number ranges from 7.90 to 9.30.