Spline approximation as applied to aeronautical problems

Ramamoorthy, P and Narayana, CL (1969) Spline approximation as applied to aeronautical problems. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    In some problems of Aeronautics such as the analysis of pressure data obtained from the wind tunnel testing on wing models or the determination of tie boundary layer characteristics from a known pressure distribution on an aerofoil one encounters with the interpolation, differentiation and integration of a functvon (eg. pressure) given at unequal intervals. Techniques available in practice such as hand fairing, series of equivalent rectangles, least-square polynomial fits and cubic curve fits give crude results* This report presents a new method based on spline approximation which gives very accurate and reliable results compared with any of the methods available now. The method is programmed for the NAL sirius computer.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Spline approximation;Determination;Variable-sweep;Mach number;Equivalent rectangles;Least-square
    Subjects: AERONAUTICS > Aeronautics (General)
    Division/Department: Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 19 Dec 2006
    Last Modified: 24 May 2010 09:54
    URI: http://nal-ir.nal.res.in/id/eprint/3780

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