A refined structural model for static aeroelastic response and divergence of metallic and composite wings
Author:
Publisher
Springer Science and Business Media LLC
Subject
Aerospace Engineering,Transportation
Link
http://link.springer.com/content/pdf/10.1007/s13272-013-0063-2.pdf
Reference48 articles.
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3. Bhatia, M., Kapania, R.K., Van Hoek, M., Haftka, R.T.: Structural design of a truss braced wing: potential and challenges. In: 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA Paper 2009-2147, Palm Springs (2009)
4. Demasi, L., Livne, E.: Aeroelastic coupling of geometrically nonlinear structures and linear unsteady aerodynamics: two formulations. J. Fluids Struct. 25(5), 918–935 (2009)
5. Demasi, L., Livne, E.: Dynamic aeroelasticity of structural nonlinear configurations using linear modally reduced aerodynamic generalized forces. AIAA J. 47(1), 71–90 (2009)
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