Fluid–structure interaction modelling of nonlinear aeroelastic structures using the finite element corotational theory
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering
Reference49 articles.
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3. Balmer, H., Witmer, E., 1964. Theorethical-experimental correlation of large dynamic and permanent deformation of impulsively loaded simple structures. Technical Report FDP-TDR-64-108, Air Force Dynamics Laboratory, Wright Patterson AFB, OH, USA.
4. Explicit algorithms for the nonlinear dynamics of shells;Belytschko;Computer Methods in Applied Mechanics and Engineering,1984
5. Bennet, R., Desmarais, R., 1975. Curve fitting of aeroelastic transient response data with exponential functions, Flutter testing techniques. NASA SP-415, pp. 43–58.
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