PIV study of end wall flow in the plane of symmetry of surface mounted obstacles of various aspect ratios

M. Javed Khan, David J. Lyons

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

Abstract

Flow visualization and PIV measurements were carried out in the plane of symmetry of end-wall region upstream of surface mounted cylinders with circular and square cross sections. The influence of aspect ratio was documented on the vortex system in this flow region for a laminar approach boundary layer. The primary vortex for a circular cylinder was observed to have larger voracity while the primary vortex for the square cylinder was observed to be farther upstream. The vortex systems were steady only for aspect ratio of 0.5 for both cases. For aspect ratios of 1.0 and 1.5 the vortex system showed an oscillatory behavior for both cylinders. The square cylinder vortex system exhibited higher frequency and amplitude of oscillation.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - 24th AIAA Applied Aerodynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages1825-1833
Number of pages9
ISBN (Print)1563478129, 9781563478123
DOIs
StatePublished - Jan 1 2006
Event24th AIAA Applied Aerodynamics Conference - San Francisco, CA, United States
Duration: Jun 5 2006Jun 8 2006

Publication series

NameCollection of Technical Papers - AIAA Applied Aerodynamics Conference
Volume3
ISSN (Print)1048-5953

Conference

Conference24th AIAA Applied Aerodynamics Conference
CountryUnited States
CitySan Francisco, CA
Period6/5/066/8/06

All Science Journal Classification (ASJC) codes

  • Engineering(all)

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