A PROJECT REPORT
Submitted by
BOOBALAKANNAN.S (090101115071)
GUNA.S (090101115077)
MOHAMED RASIK FAREETH.M (090101115088)
VIJAYA KUMAR.J (090101115117)
In partial fulfillment for the award of the degree
Of
BACHELOR OF ENGINEERING
In
AERONAUTICAL ENGINEERING
NEHRU INSTITUTE OF ENGINEERING AND TECHNOLOGY,
COIMBATORE.
ANNA UNIVERSITY
CHENNAI 600025
MAY 2013
ANNA UNIVERSITY CHENNAI 600025
BONAFIDE CERTIFICATE
Certified that this project report “AERODYNAMIC ANALYSIS OF MULTI-WINGLET FOR LOWSPEED AIRCRAFT’’ is the bonafide work of
BOOBALAKANNAN.S (090101115071)
GUNA.S (090101115077)
MOHAMED RASIK FAREETH.M (090101115088)
VIJAYA KUMAR.J (090101115117)
Who carried out the project under my supervision.
SIGNATURE SIGNATURE
Mr.E.DILEEP. B.E Mr. B.R.SENTHIL KUMAR. M.E
SUPERVISOR HEAD OF THE DEPARTMENT
Lecturer Dept. of Aeronautical Engg
Dept. of Aeronautical Engg NIET, Coimbatore–641105
NIET, Coimbatore - 641105
…………………… ...................................
Internal Examiner External Examiner
ACKNOWLEDGEMENT We wish to express our deep gratitude and sincere thanks to our NGI management for providing all facilities needed in the preparation of this project. We are very much grateful to our secretary Dr.P.Krishnakumar, M.B.A., M.Phil., Ph.D., and our principal Dr.P.Maniiarasan, M.E., Ph.D., for their kind permission and encouragement for completing this project. We also thank our director Dr.S.R.Balakrishnan, Ph.D., as the faculty member for being project discussions giving suggestions and helping us to improve our project. We extend our gratitude to Mr.B.R.Senthil Kumar, M.E., Head of the Department, Aeronautical Engineering, for his kind support. We express our thanks to our Academic Coordinator Mr.N.Balaji, B.E., for his guidance in all matters
References: Drag reduction in aircraft winglet using Elliptical wing. (Prithvi Raj Aurora, A. Husain, Prasetyo Edi, A.A. Jaafar, Thamir S. Younis and M. Saleem).Journal - The Institution of Engineers, Malaysia (Vol. 66, No. 4, December 2005). Design of multiple winglets to improve turning and soaring characteristics of ANGELO D’ARRIGO’S HANGGLIDER : NUMERICAL AND EXPERIMENTAL INVESTIGATION. D. P. COIRO, F. NICOLOSI , F. SCHERILLO, U. MAISTO. SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION D. P. Coiro, F. Nicolosi, F. Scherillo, U. Maisto.(Department of Aerospace Engineering (DIAS), University of Naples “Federico II”, 80125,Naples, Italy). CFD Analysis of Winglets at Low Subsonic Flow M. A Azlin, C.F Mat Taib, S. Kasolang and F.H Muhammad Proceedings