Direct solution of two-dimensional Navier-Stokes equations for static aeroelasticity problems
- 1 January 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (1) , 148-153
- https://doi.org/10.2514/3.11331
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Newton's method applied to finite-difference approximations for the steady-state compressible Navier-Stokes equationsJournal of Computational Physics, 1991
- Integrated aerodynamic-structural design of a transport wingJournal of Aircraft, 1990
- Static aeroelastic analysis of fighter aircraft using a three-dimensional Navier-Stokes algorithmJournal of Aircraft, 1990
- Unsteady aerodynamic and aeroelastic calculations for wings using Euler equationsAIAA Journal, 1990
- Static aeroelasticityPublished by Springer Nature ,1989
- The solution of the Navier-Stokes equations using Gauss-Seidel line relaxationComputers & Fluids, 1989
- A finite-element study of the onset of vortex shedding in flow past variously shaped bodiesJournal of Fluid Mechanics, 1987
- Application of MACSYMA and sparse matrix technology to multielement airfoil calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Steady viscous flow past a circular cylinder up to reynolds number 600Journal of Computational Physics, 1985
- Finite-difference methods for computing the steady flow about blunt bodiesJournal of Computational Physics, 1980