Preview

Multiwinglets

Powerful Essays
Open Document
Open Document
5788 Words
Grammar
Grammar
Plagiarism
Plagiarism
Writing
Writing
Score
Score
Multiwinglets
AERODYNAMIC ANALYSIS OF MULTI-WINGLET FOR LOW SPEED AIRCRAFT
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

You May Also Find These Documents Helpful

  • Better Essays

    [2] Queen Mary University of London, DEN233, Low Speed Aerodynamics, Lecture Notes, 2013, (Accessed on 13th November 2013)…

    • 2962 Words
    • 12 Pages
    Better Essays
  • Better Essays

    As a result of the experiment and computation of data, the aerofoil was found to have a critical Mach number of M=0.732. Below this freestream Mach number the Prandtl-Glauert law predicted results very successfully. However, above this value, the law completely breaks down. This was found to be the result of local regions of supersonic flow and local shockwaves.…

    • 2069 Words
    • 9 Pages
    Better Essays
  • Better Essays

    introduction

    • 5346 Words
    • 41 Pages

    Anderson JD Jr. 1997. A History of Aerodynamics and Its Impact on Flying Machines. London: Cambridge Univ. Press.…

    • 5346 Words
    • 41 Pages
    Better Essays
  • Powerful Essays

    Capstone

    • 4523 Words
    • 13 Pages

    The purpose of this research paper is show that winglets have benefits and drawbacks, and that the airliners that are currently using these devices have a competitive advantage compared to an airliner without winglets. Since the first winglet were first installed in 1977, on a LearJet 28. These small aerodynamic devices have proven to be beneficial and also have drawbacks. Winglets have since proven to save airliners and private owners thousands of dollars, but these devices due not come cheap. This paper will discuss how winglets have benefits and drawbacks that are proven to be more beneficial in the long run. Also this paper will discuss that having winglets are beneficial and airliners that are installing winglets have reduced their fuel consumption as early as 2000. Finally, this project will conclude that winglets do not just benefit a plane in its fuel consumption, but are enhancing the aircrafts performance with mileage and reducing cost for those that are flying within the plane.…

    • 4523 Words
    • 13 Pages
    Powerful Essays
  • Better Essays

    Asci 202

    • 1008 Words
    • 5 Pages

    A rotorcraft’s fuselage or structure must be strong and light weight while its flight controls agile and reliable. The type of rotor system designed is very important as well. There are two types commonly found on rotary-wing aircraft today. They are a fully articulated or semi-rigid under slung see saw type rotor system. Both have their own advantages and dis-advantages over the other. The fully articulated rotor system is complex by design, it has excellent control authority in the pitch and roll axis. It also typically has more than two rotor blades which reduces sound signature and increases control authority in the pitch and roll axis controlled by the cyclic due to its solidity ratio. The semi-rigid rotor system is a much simpler design thus, it cost significantly less to maintain but control authority in the pitch and roll axis is sluggish compared to the fully articulated rotor system due to its lower solidity ratio.…

    • 1008 Words
    • 5 Pages
    Better Essays
  • Better Essays

    Physics of Airplanes

    • 1550 Words
    • 7 Pages

    Cited: Sanders. "AERODYNAMICS AND THEORY OF FLIGHT." Aerodynamics and Theory of Flight Langley Flying School. N.p., May 2008. Web. 19 Mar. 2013.…

    • 1550 Words
    • 7 Pages
    Better Essays
  • Best Essays

    Boeing Report

    • 2380 Words
    • 10 Pages

    Chris Brady. 1999. Advanced Blended / Advanced Technology Winglets. [ONLINE] Available at:http://www.b737.org.uk/winglets.htm. [Accessed 04 March 13].…

    • 2380 Words
    • 10 Pages
    Best Essays
  • Better Essays

    References: Bond, D. (07/18/2005). Big Mo at Southwest. Aviation Week & Space Technology, 163(3), p36. Retrieved from http://search.ebscohost.com.ezproxy.apollolibrary.com/login.aspx?direct=true&db=f5h&AN=17739259&site=ehost-live…

    • 1271 Words
    • 6 Pages
    Better Essays
  • Powerful Essays

    Dynamics

    • 1951 Words
    • 8 Pages

    In the present case the motion is unidimensional and the force produce by a weight of m1 is | RF | = m1 · | Rg | ; m1 · g where g is the acceleration of gravity. If the total mass of the glider is m2 the equation of motion is given by (m2 + m1) · | Ra | = m1 · g ; (1) The velocity is | Rv (t) | ; v= · t (2) and the position is | Rr (t) | ; s (t) = · t 2. (3)…

    • 1951 Words
    • 8 Pages
    Powerful Essays
  • Powerful Essays

    Timeline of airplanes

    • 1770 Words
    • 7 Pages

    German professor Ludwig Prandtl presents one of the most important papers in the history of aerodynamics, an eight-page document describing the concept of a fixed "boundary layer," the molecular layer of air on the surface of an aircraft wing. Over the next 20 years Prandtl and his graduate students pioneer theoretical aerodynamics.…

    • 1770 Words
    • 7 Pages
    Powerful Essays
  • Better Essays

    Southwest Airline

    • 1110 Words
    • 5 Pages

    - Outfit the fleet with fuel-saving, performance-enhancing blended winglet that extend flight range, save fuel, and reduce engine maintenance costs and takeoff noise.…

    • 1110 Words
    • 5 Pages
    Better Essays
  • Better Essays

    Module 2). Aluminum alloys are preferred due to their high strength, low weight and relatively…

    • 1721 Words
    • 7 Pages
    Better Essays
  • Good Essays

    Winglets have multiple design purposes. They are cambered so that the wingtip vortices rotating from below the wing strike the surface of the…

    • 973 Words
    • 4 Pages
    Good Essays
  • Good Essays

    A tandem wing aircraft has two main wings, with one located forward and the other to the rear, both wings contribute to lift. A lower first wing is located at the forward end of the fuselage attached directly to fuselage structure. A second higher wing is located at the aft end of the fuselage. Pitch control is achieved by increasing or decreasing the lift on either wing. In a tandem wing design the lift vectors on the two wings are spread far apart longitudinally, allowing them to act together to achieve stability and control.…

    • 7425 Words
    • 48 Pages
    Good Essays
  • Good Essays

    Aircraft Winglets

    • 2752 Words
    • 12 Pages

    Many of us who fly regularly have most probably seen a so-called winglet or wingtip device at the end of the wing of an airliner at least once. It is showing up more and more often on more and more types of aircraft, thus we felt it’s time to give an overview to our readers about these sometimes funny, sometimes cool and stylish looking aircraft parts.…

    • 2752 Words
    • 12 Pages
    Good Essays

Related Topics