Design of a Natural laminar Flow Airfoil for a Regional Transport Aircraft

Srilatha, KR and Ramamoorthy, P (1990) Design of a Natural laminar Flow Airfoil for a Regional Transport Aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    A 16% thick NLF airfoil is designed for a future regional13; aircraft which is expected to incorporate advance technology13; concepts in Aerodynamics, structures and Controls. This airfoil13; is compared with DO-NTLF-160 airfoil of same thickness. . .13; NAL airfoil, designated as. NAL-MSNLF-160, has given the same13; Performance as NTLF airfoil if not better.13; 13;

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Airfoil;Design;Pressure Distribution;General13; Aviation;Regional Transport.13; 13;
    Subjects: AERONAUTICS > Aircraft Propulsion and Power
    Division/Department: Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division
    Depositing User: Mrs Manoranjitha M D
    Date Deposited: 15 Jul 2006
    Last Modified: 24 May 2010 09:45
    URI: http://nal-ir.nal.res.in/id/eprint/2074

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