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.

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

Download (436Kb)

    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: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Aerodynamic influence coefficients;Supersonic flow;Finite element;Boolean matrix
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 25 Jan 2007
    Last Modified: 24 May 2010 09:52
    URI: http://nal-ir.nal.res.in/id/eprint/3265

    Actions (login required)

    View Item