Aeroplane Wing Flutter: A Detailed Discussion of Measures for the Avoidance of Unstable Oscillation of Aeroplane Wings
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 April 1929
Abstract
FOR all stiffness ratios, there is clearly a marked increase of critical speed when the centre of inertia is as far forward as the flexural centre.
Citation
Frazer, R.A. (1929), "Aeroplane Wing Flutter: A Detailed Discussion of Measures for the Avoidance of Unstable Oscillation of Aeroplane Wings", Aircraft Engineering and Aerospace Technology, Vol. 1 No. 4, pp. 138-145. https://doi.org/10.1108/eb029138
Publisher
:MCB UP Ltd
Copyright © 1929, MCB UP Limited