Flutter analysis of a viscoelastic tapered wing under bending–torsion loading

Author:

Matter Youssef S.,Darabseh Tariq T.,Mourad Abdel-Hamid I.

Funder

United Arab Emirates University

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference34 articles.

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2. Abdelkefi A, Vasconcellos R, Nayfeh AH, Hajj MR (2013) An analytical and experimental investigation into limit-cycle oscillations of an aeroelastic system. Nonlinear Dyn 71(159):173

3. Abdelkefi A, Vasconcellos R, Marques FD, Hajj MR (2012) Modeling and identification of freeplay nonlinearity. J Sound Vib 331:1898–1907

4. Acum WEA (1959) The comparison of theory and experiment of oscillating wings, vol. II, chpater 10, AGARD manual on aeroelasticity

5. Baker WE, Woolam WE, Young D (1967) Air and internal damping of thin cantilever beams. Int J Mech Sci 9:743–766

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