Modeling of Airfoil Trailing Edge Flap with Immersed Boundary Method

Research output: Chapter in Book/Report/Conference proceedingArticle in proceedingsResearchpeer-review

501 Downloads (Pure)

Abstract

The present work considers incompressible flow over a 2D airfoil with a deformable trailing edge. The aerodynamic characteristics of an airfoil with a trailing edge flap is numerically investigated using computational fluid dynamics. A novel hybrid immersed boundary (IB) technique is applied to simulate the moving part of the trailing edge. Over the main fixed part of the airfoil the Navier-Stokes (NS) equations are solved using a standard body-fitted finite volume technique whereas the moving trailing edge flap is simulated with the immersed boundary method on a curvilinear mesh. The obtained results show that the hybrid approach is an efficient and accurate method for solving turbulent flows past airfoils with a trailing edge flap and flow control using trailing edge flap is an efficient way to regulate the aerodynamic loading on airfoils.
Original languageEnglish
Title of host publicationICOWEOE-2011
VolumePaper 07
Publication date2011
Publication statusPublished - 2011
EventInternational Conference on Offshore Wind Energy and Ocean Energy - Beijing, China
Duration: 31 Oct 20112 Nov 2011

Conference

ConferenceInternational Conference on Offshore Wind Energy and Ocean Energy
CountryChina
CityBeijing
Period31/10/201102/11/2011

Cite this