Vortical flow computations on a flexible blended wing-body configuration
- 1 October 1992
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (10) , 2497-2503
- https://doi.org/10.2514/3.11252
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Streamwise upwind algorithm for computing unsteady transonic flows past oscillating wingsAIAA Journal, 1991
- Ensaero—A multidisciplinary program for fluid/structural interaction studies of aerospace vehiclesComputing Systems in Engineering, 1990
- Unsteady aerodynamic and aeroelastic calculations for wings using Euler equationsAIAA Journal, 1990
- Computation of turbulent supersonic flows around pointed bodies having crossflow separationJournal of Computational Physics, 1986
- 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