Comparison of two candidate airfoils for LTA application

Rajana, BN and Viswanathan, S (1995) Comparison of two candidate airfoils for LTA application. Technical Report. National Aerospace Laboratories, Bangalore, India.

Full text available as:
[img] PDF
Restricted to Archive staff only

Download (2331Kb)

    Abstract

    This report pertains to a comparative study of the performance of GAW-2 airfoil against the one designed by TSAGI for application to civil aircraft. Performance of teh two airfoils are evaluated in terms of lift coefficient, pitching moment, drag and chordwise pressure distribution. All these quantities are computed using extensively validated NGSU and DLR codes.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: airfoil; pressure distribution; drag; lift; pitching moment
    Subjects: ENGINEERING > Fluid Mechanics and Thermodynamics
    Division/Department: Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division
    Depositing User: Smt Bhagya Rekha KA
    Date Deposited: 28 Jan 2006
    Last Modified: 24 May 2010 09:39
    URI: http://nal-ir.nal.res.in/id/eprint/932

    Actions (login required)

    View Item