Kinametically consistent unsteady aerodynamic coefficients13; in supersonic flow Part I : Theoretical basis

Kariappa, - (1968) Kinametically consistent unsteady aerodynamic coefficients13; in supersonic flow Part I : Theoretical basis. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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Abstract

A finite element approach to determine the aerodynamic influence coefficients consistent with the stiffness and inertia properties of a flying vehicle in supersonic13; flow is presented. This is basically a kinematic method which reduces the dynamical equations of a nonconservative system to a simple and elegant form. This approach amalgamates the disciplines of matrix algebra, and is essentially suitable for a modern high speed digital computer.

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Aerodynamic influence coefficients;Supersonic flow;Finite element;Boolean matrix
Subjects: AERONAUTICS > Aerodynamics
Depositing User: Users 90 not found.
Date Deposited: 25 Jan 2007
Last Modified: 24 May 2010 04:22
URI: http://nal-ir.nal.res.in/id/eprint/3265

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