Development of a finite element aeroelastic analysis capability
- 1 September 1996
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 33 (5) , 995-1002
- https://doi.org/10.2514/3.47046
Abstract
No abstract availableKeywords
This publication has 21 references indexed in Scilit:
- Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler methodAIAA Journal, 1993
- WING FLUTTER BOUNDARY PREDICTION USING UNSTEADY EULER AERODYNAMIC METHODPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- AN OVERVIEW OF AEROELASTICITY STUDIES FOR THE NATIONAL AERO-SPACE PLANEPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Vortical flow computations on a flexible blended wing-body configurationAIAA Journal, 1992
- Aeroelastic analysis of wings using the Euler equations with a deforming meshJournal of Aircraft, 1991
- A new approach to computational aeroelasticityPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Unsteady Euler algorithm with unstructured dynamic mesh for complex-aircraft aerodynamic analysisAIAA Journal, 1991
- Adaptive H-refinement on 3-D unstructured grids for transient problemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Time-accurate unsteady aerodynamic and aeroelastic calculations for wings using Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Unsteady full potential aeroelastic computations for flexible configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987