h-Adaptive Stabilized Finite-Element Solver for Calculation of Generalized Aerodynamic Forces-Reference-Cited by-同舟云学术

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

Published:2015-03 Issue:3 Volume:53 Page:554-572
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

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

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053128

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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