Influence of aerodynamic nonlinearity due to static panel-curvature on flutter of panels at transonic and low supersonic Mach numbers
Author:
Funder
Ohio Aerospace Institute
Air Force Office of Scientific Research
Publisher
Elsevier BV
Subject
Mechanical Engineering
Reference23 articles.
1. A parametric study on supersonic/hypersonic flutter behavior of aero-thermo-elastic geometrically imperfect curved skin panel;Abbas;Acta Mech.,2011
2. Review of unsteady transonic aerodynamics theory and applications;Bendiksen;Prog. Aerosp. Sci.,2011
3. Bhatia, M., 2016. MAST web page. https://github.com/MASTmultiphysics/mast-multiphysics.
4. h-Adaptive stabilized finite-element solver for calculation of generalized aerodynamic forces;Bhatia;AIAA J.,2015
5. Design of thermally stressed panels subject to transonic flutter constraints;Bhatia;J. Aircr.,2017
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