Tail Flutter—A New Theory: In which is Discussed in Some Detail the Structural Instability of Tail Planes at High Speed
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 January 1929
Abstract
THE stresses existing in the structure of a tail plane, in varying conditions of flight, are possibly more a matter of doubt than obtains for any other part of an aeroplane structure. The assumptions made at present are frankly conventional, but are accepted because in the past they have usually yielded satisfactory results.
Citation
Bolas, H. (1929), "Tail Flutter—A New Theory: In which is Discussed in Some Detail the Structural Instability of Tail Planes at High Speed", Aircraft Engineering and Aerospace Technology, Vol. 1 No. 1, pp. 16-22. https://doi.org/10.1108/eb029094
Publisher
:MCB UP Ltd
Copyright © 1929, MCB UP Limited