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: Monograph (Technical Report)
Uncontrolled Keywords: Wagner;Finite wing;Pseudo orthonormal property;Differential equation
Subjects: AERONAUTICS > Aerodynamics
Depositing User: M/S ICAST NAL
Date Deposited: 22 Dec 2006
Last Modified: 24 May 2010 04:24
URI: http://nal-ir.nal.res.in/id/eprint/3723

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