Aerodynamic Boundary Layer Effects on Flutter and Damping of Plates
- 1 December 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 10 (12) , 734-738
- https://doi.org/10.2514/3.60298
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Generalized aerodynamic forces on a flexible plate undergoing transient motion in a shear flow with an application to panel flutterAIAA Journal, 1971
- SOME RECENT CONTRIBUTIONS TO PANEL FLUTTER RESEARCHAIAA Journal, 1963
- REFLECTION AT A LAMINAR BOUNDARY LAYER OF A WEAK STEADY DISTURBANCE TO A SUPERSONIC STREAM, NEGLECTING VISCOSITY AND HEAT CONDUCTIONThe Quarterly Journal of Mechanics and Applied Mathematics, 1950