Application of forced unsteady aerodynamics to a forward swept wing X-29 model
- 11 January 1988
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Visualization of wing tip vortices in accelerating and steady flowJournal of Aircraft, 1986
- The vortex patterns of dynamic separation: A parametric and comparative studyProgress in Aerospace Sciences, 1985
- X-29 forward swept wing aerodynamic overviewPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Wind tunnel investigation of the transonic aerodynamic characteristics of forward swept wingsJournal of Aircraft, 1983