Application of a three-field nonlinear fluid–structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter-Reference-Cited by-同舟云学术

Application of a three-field nonlinear fluid–structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter

Published:2003-01 Issue:1 Volume:32 Page:3-29
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Farhat Charbel,Geuzaine Philippe,Brown Gregory

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference37 articles.

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3. An approximate true damping solution of the flutter equation by determinant iteration;Hassig;J Aircraft,1971

4. A doublet-lattice method for calculating lift distribution on oscillating surfaces in subsonic flow;Albano;AIAA J,1969

5. Piston theory––a new aerodynamic tool for the aeroelastician;Ashley;J Aero Sci,1956

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