Vortical flow computations on swept flexible wings using Navier-Stokes equations
- 1 December 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (12) , 2077-2084
- https://doi.org/10.2514/3.10524
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Unsteady aerodynamic and aeroelastic calculations for wings using Euler equationsAIAA Journal, 1990
- Numerical simulation of vortical flows on flexible wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- The numerical simulation of transonic separated flow about the complete F-16APublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Unsteady surface pressure measurements on a pitching rectangular wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Numerical simulations of unsteady, viscous, transonic flow over isolated and cascaded airfoils using a deforming gridPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Transonic aeroelastic analysis of the B-1 wingJournal of Aircraft, 1986
- SELF-INDUCED OSCILLATION WIND TUNNEL TEST OF A VARIABLE SWEEP WINGPublished by American Institute of Aeronautics and Astronautics (AIAA) ,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
- An implicit finite-difference algorithm for hyperbolic systems in conservation-law formJournal of Computational Physics, 1976