Limit cycle phenomena in computational transonic aeroelasticity
- 1 November 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 31 (6) , 1257-1263
- https://doi.org/10.2514/3.46644
Abstract
No abstract availableKeywords
This publication has 18 references indexed in Scilit:
- Limit cycle phenomena in computational transonic aeroelasticityPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Nonlinear aspects of the transonic aeroelastic stability problemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Transonic flutter analysis using the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Effects of structural nonlinearities on limit cycle response of aerodynamic surfacesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- An iterative procedure for nonlinear flutter analysisAIAA Journal, 1986
- Experimental and Theoretical Study of Nonlinear FlutterJournal of Aircraft, 1981
- Transonic dip mechanism of flutter of a sweptback wing. IIAIAA Journal, 1981
- On the Transonic-Dip Mechanism of Flutter of a Sweptback WingAIAA Journal, 1979
- An Approximate Analysis of Nonlinear Flutter ProblemsJournal of the Aerospace Sciences, 1959
- An Investigation of Effects of Certain Types of Structural NonHnearities on Wing and Control Surface FlutterJournal of the Aeronautical Sciences, 1957