Experimental Determination of the Centre-of-Flexure and Centre-of-Torsion Co-Ordinates of an Asymmetrical Aerofoil Cross-Section
- 1 December 1959
- journal article
- Published by SAGE Publications in Journal of Mechanical Engineering Science
- Vol. 1 (3) , 241-249
- https://doi.org/10.1243/jmes_jour_1959_001_029_02
Abstract
The differential equations of motion (1)† of a vibrating cantilever blade contain coupling terms dependent upon the co-ordinates of the centre-of-flexure relative to the centroid of the blading cross-section. Complete solution of the equations, therefore, requires a knowledge of the co-ordinates.Keywords
This publication has 2 references indexed in Scilit:
- Vibrations of Pre-Twisted Cantilever BladingProceedings of the Institution of Mechanical Engineers, 1959
- XV.The flexural centre and the centre of twist of an elastic cylinderJournal of Computers in Education, 1933