Numerical investigation of a jet and vortex actuator in a cross flow boundary layer

Sertac Cadirci*, Hasan Gunes, Ulrich Rist

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

11 Citations (Scopus)

Abstract

The performance of a zero-net-mass-flux Jet and Vortex Actuator (JaVA) was numerically investigated in a two-dimensional-cross-flow flat-plate laminar boundary layer. The JaVA is an active flow control device that can be used for flow separation control and thus can delay/prevent boundary layer separation. In this study, an unsteady, incompressible flow solver has been used to study the flow fields generated by a JaVA in a water channel. Detailed quantitative information about the performance of the JaVA on a flat-plate boundary layer is obtained. JaVA-induced boundary-layer profiles are clearly 'fuller' at the wall and hence more resistant to flow separation. The 'positive' effects of the JaVA with different operating regimes on various boundary-layer flow characteristics such as displacement thickness, shape factor and the friction coefficient are presented in this study. Selecting the appropriate governing parameters in conjunction with cross-flow properties, the velocity profile can be tuned in a boundary layer to delay or prevent separation.

Original languageEnglish
Pages (from-to)42-59
Number of pages18
JournalEuropean Journal of Mechanics, B/Fluids
Volume44
DOIs
Publication statusPublished - 2014

Funding

We gratefully acknowledge the financial support of the Scientific and Technological Research Council of Turkey (TÜBİTAK) and the International Bureau of the Federal Ministry of Education and Research (BMBF), Germany through the project Development and Testing of a Jet and Vortex Actuator (JaVA) for Active Flow Control, Nr. 107M644 and TUR 07/006 , respectively.

FundersFunder number
Bundesministerium für Bildung und Forschung
Türkiye Bilimsel ve Teknolojik Araştirma Kurumu

    Keywords

    • Active flow control
    • Boundary layer
    • Computational fluid dynamics
    • Dynamic mesh
    • Jet and vortex actuator
    • Zero-net-mass-flux

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