Application of CFD simulation in the design of a parabolic winglet on NACA 2412

Arvind Prabhakar, Ayush Ohri

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

1 Citation (Scopus)

Abstract

Winglets are angled extensions or vertical projections at the tip of a wing, they are widely used in conjunction with plain airfoils on commercial airplanes for the purpose of reducing induced drag, vortices, and increasing lift. In this paper parabolic shaped configuration winglets at cant angles 45 and 55 degrees are analyzed on rectangular NACA 2412 airfoil sections using CFD analysis at Reynolds number 2*105 and 4*105 to compare aerodynamic characteristics. The wing is of 6 inch chord and 12 inches span, airfoils have been created using CATIA V5 and CFD analysis has been carried out using commercial code software ANSYS FLUENT 14.0, it is found that the L/D ratio increases by 13.447% and the coefficient of lift (CL) increases by 1.958% for a parabolic winglet at 45 degrees cant angle at 2*105 Reynolds number causing a maximum reduction in coefficient of drag (CD) by 10.125% and thereby reducing fuel consumption of the aircraft.

Original languageEnglish
Title of host publicationWorld Congress on Engineering, WCE 2014
PublisherNewswood Limited
Pages1224-1231
Number of pages8
Volume2
ISBN (Print)9789881925350
Publication statusPublished - 01-01-2014
Externally publishedYes
EventWorld Congress on Engineering, WCE 2014 - London, United Kingdom
Duration: 02-07-201404-07-2014

Conference

ConferenceWorld Congress on Engineering, WCE 2014
CountryUnited Kingdom
CityLondon
Period02-07-1404-07-14

All Science Journal Classification (ASJC) codes

  • Computer Science (miscellaneous)

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