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: | 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 |
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