Structure-attached corotational fluid grid for transient aeroelasticcomputations
- 1 March 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (3) , 597-599
- https://doi.org/10.2514/3.11371
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Unsteady Euler airfoil solutions using unstructured dynamic meshesPublished 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
- Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional GeometriesAIAA Journal, 1978