Derivation of four-digit airfoils from the Sunya airfoil

Ramamoorthy, P (1997) Derivation of four-digit airfoils from the Sunya airfoil. Journal of aircraft, 34 (3). pp. 441-443. ISSN 0021-8669

Full text available as:
[img] PDF
Restricted to CSIR-NAL Registered users only

Download (885Kb)


    A class of four-digit airfoil profiles is obtained on the basis of Ramamoorthy's (1995) 'Sunya' airfoil analytical representation. It is shown that the Sunya airfoil, described by a simple analytical expression, may be considered as a standard for all single-parameter airfoils.

    Item Type: Journal Article
    Additional Information: Copyright for this article belongs to AIAA
    Uncontrolled Keywords: Airfoil profiles;Thickness ratio;Chords(geometry);Airfoils;Velocity distribution;Coordinates
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Computational and Theoretical Fluid Dynamics Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 03 Mar 2010
    Last Modified: 24 May 2010 09:51

    Actions (login required)

    View Item