Velocity field around a rigid flapping wing with a winglet in quiescent water

Srikanth Goli*, Arnab Roy, Subhransu Roy

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

2 Scopus citations

Abstract

This study investigated the effect of a winglet on the velocity field around a rigid flapping wing. Two-dimensional particle image velocimetry was used to capture the velocity field of asymmetric one-degree-of-freedom flapping motion. A comparison was conducted between wings with and without a winglet at two flapping frequencies, namely 1.5 and 2.0 Hz. The effect of the winglet on the velocity field was determined by systematically comparing the velocity fields for several wing phase angles during the downstroke and upstroke. The presence of a winglet considerably affected the flow field around the wingtip, residual flow, and added mass interaction. The added mass was lower and residual flow was weaker for the wings with a winglet than for the wings without a winglet. The added mass and velocity magnitudes of the flow field increased proportionally with the flapping frequency.

Original languageEnglish
Pages (from-to)259-269
Number of pages11
JournalAdvances in Technology Innovation
Volume5
Issue number4
DOIs
StatePublished - Sep 2020
Externally publishedYes

Bibliographical note

Publisher Copyright:
© by the authors.

Keywords

  • Flapping motion
  • One-degree-of-freedom flapping
  • PIV
  • Square wing
  • Velocity field
  • Winglet

ASJC Scopus subject areas

  • Management of Technology and Innovation
  • General Computer Science
  • Energy Engineering and Power Technology
  • Renewable Energy, Sustainability and the Environment
  • General Engineering
  • Environmental Engineering

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