Vortical flow computations on swept flexible wings using Navier-Stokes equations
- 3 April 1989
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Transonic aeroelastic analysis of the B-1 wingJournal of Aircraft, 1986
- Aeroelastic time response analysis of thin airfoils by transonic code LTRAN2Computers & Fluids, 1981