Control of vortex shedding from a cylinder at different sweep back angles

L. Taubert, Israel J Wygnanski

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

1 Citation (Scopus)

Abstract

The control of vortex shedding from a yawed cylinder at different sweep back angles 0°, 45° and 60°, is currently investigated at the University of Arizona. Active flow control is applied on the cylinder in the form of oscillatory, zero mass flux excitation through two slots located symmetrically on the circumference. Surface and wake pressure measurements are carried out, as well as application of flow visualization and Particle Image Velocimetry.

Original languageEnglish (US)
Title of host publication2nd AIAA Flow Control Conference
StatePublished - 2004
Event2nd AIAA Flow Control Conference 2004 - Portland, OR, United States
Duration: Jun 28 2004Jul 1 2004

Other

Other2nd AIAA Flow Control Conference 2004
CountryUnited States
CityPortland, OR
Period6/28/047/1/04

Fingerprint

Vortex shedding
Flow visualization
Engine cylinders
Pressure measurement
Flow control
Velocity measurement
Mass transfer

ASJC Scopus subject areas

  • Fluid Flow and Transfer Processes
  • Aerospace Engineering
  • Control and Systems Engineering

Cite this

Control of vortex shedding from a cylinder at different sweep back angles. / Taubert, L.; Wygnanski, Israel J.

2nd AIAA Flow Control Conference. 2004.

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

Taubert, L & Wygnanski, IJ 2004, Control of vortex shedding from a cylinder at different sweep back angles. in 2nd AIAA Flow Control Conference. 2nd AIAA Flow Control Conference 2004, Portland, OR, United States, 6/28/04.
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