Application of transonic small disturbance theory to the active flexible wing model
- 1 January 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 32 (1) , 16-22
- https://doi.org/10.2514/3.46678
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Transonic flutter analysis using the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Measured and calculated effects of angle of attack on the transonic flutter of a supercritical wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Experiments in unsteady transonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979