Estimation of drag-divergence mach number for an airfoil

Narayana, CL and Sinha, AK and Ramamoorthy, P (1976) Estimation of drag-divergence mach number for an airfoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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

Download (8Mb)


    A design software package for determining the drag divergence Mach nmilber LiD is developed. The essential method is contained in the RAE data sheets. The method make s use of the Theoderson's program for incompressible flow developed by the same group. Extensive /compsrisons are made. A simple sweep correction extends the athod to sweptback wings.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Airfoil;Drag divergence
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics, Aerodynamics
    Depositing User: Poornima Narayana
    Date Deposited: 28 Aug 2006
    Last Modified: 24 May 2010 09:48

    Actions (login required)

    View Item