Coupled bending-torsion vibrations of rotating blades of asymmetric aerofoil cross section with allowance for shear deflection and rotary inertia by use of the Reissner method
- 8 March 1981
- journal article
- Published by Elsevier in Journal of Sound and Vibration
- Vol. 75 (1) , 17-36
- https://doi.org/10.1016/0022-460x(81)90233-9
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
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