Wing-body aeroelasticity using finite-difference fluid/finite element structural equations on parallel computers
- 18 April 1994
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Fluid-structural interactions using Navier-Stokes flow equations coupled with shell finite element structuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Vortical flow computations on a flexible blended wing-body configurationAIAA Journal, 1992
- Coupled finite-difference/finite-element approach for wing-body aeroelasticityPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Finite-surface splineJournal of Aircraft, 1989
- A parallel finite element solution methodComputers & Structures, 1986
- The determination of load and slope transformation matrices for aeroelastic analysisJournal of Aircraft, 1985
- Aeroelastic time response analysis of thin airfoils by transonic code LTRAN2Computers & Fluids, 1981
- A diagonal form of an implicit approximate-factorization algorithmJournal of Computational Physics, 1981
- Interpolation using surface splines.Journal of Aircraft, 1972
- A Method of Computation for Structural DynamicsJournal of the Engineering Mechanics Division, 1959