Wagner functions

Ramamoorthy, P and Dwarakanath, GS and Narayana, CL (1969) Wagner functions. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Wagner introduced a set of functions, henceforth to be called quot;Wagner functionsquot;, in approximating the pressure load on a finite wing in the chord wise direction. It is shown that these functions form a linearly independent set satisfying quot;Pseudo orthonormal propertyquot; with respect to a suitable weighting function and further their properties such as die recurrence relation, the differential equation, generating function etc., are derived.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Wagner;Finite wing;Pseudo orthonormal property;Differential equation
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics, Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 22 Dec 2006
    Last Modified: 24 May 2010 09:54
    URI: http://nal-ir.nal.res.in/id/eprint/3723

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