h-Adaptive Stabilized Finite-Element Solver for Calculation of Generalized Aerodynamic Forces

Author:

Bhatia Manav1,Beran Philip1

Affiliation:

1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Dayton, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference62 articles.

1. Piston Theory-A New Aerodynamic Tool for the Aeroelastician

2. Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow

3. McNamaraJ. J. “Aeroelastic and Aerothermoelastic Behavior of Two and Three Dimensional Lifting Surfaces In Hypersonic Flow,” Ph.D. Thesis, Dept. of Aerospace Engineering, Univ. of Michigan, Ann Arbor, MI, Nov. 2005.

4. Flutter Boundary Identification for Time-Domain Computational Aeroelasticity

5. Review of unsteady transonic aerodynamics: Theory and applications

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