Transonic Flutter Analysis of a Rectangular Wing with Conventional Airfoil Sections
- 1 October 1980
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (10) , 1159-1164
- https://doi.org/10.2514/3.50866
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
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- A finite difference method for the solution of the transonic flow around harmonically oscillating wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Computation of Transonic Flow about Finite Lifting WingsAIAA Journal, 1972
- Calculation of plane steady transonic flowsAIAA Journal, 1971
- A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.AIAA Journal, 1969
- The Flutter of a Uniform Cantilever WingJournal of Applied Mechanics, 1945