Transonic aeroelastic analysis of the B-1 wing
- 1 July 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 23 (7), 547-553
- https://doi.org/10.2514/3.45342
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Effects of viscosity and modes on transonic aerodynamic and aeroelastic characteristics of wingsJournal of Aircraft, 1985
- SELF-INDUCED OSCILLATION WIND TUNNEL TEST OF A VARIABLE SWEEP WINGPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- An efficient coordinate transformation technique for unsteady, transonic aerodynamic analysis of low aspect-ratio wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Computations and aeroelastic applications of unsteady transonic aerodynamics about wingsJournal of Aircraft, 1984
- Some recent applications of XTRAN3SPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Flutter analysis of a transport wing using XTRAN3SPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Aeroelastic time response analysis of thin airfoils by transonic code LTRAN2Computers & Fluids, 1981
- Implicit Finite-Difference Computations of Unsteady Transonic Flows about AirfoilsAIAA Journal, 1977