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Semi‐Cantilever Wings: A Mathematical Analysis, Checked by Experimental Tests, of the Free Oscillations in the System

C. Pasqualini (Member of the staff of the National University and of the Military Aeroplane Factory, Córdoba, Argentina)
D. Biro (Member of the staff of the National University and of the Military Aeroplane Factory, Córdoba, Argentina)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 November 1935

Abstract

IN the following, the free flexional oscillations of a monoplane's semi‐cantilever wing are given, taking into consideration the inner and outer parts of the strut as two systems coupled by elasticity. The result, which is identical with coupled electrical circuits, has been checked by tests with a light aeroplane.

Citation

Pasqualini, C. and Biro, D. (1935), "Semi‐Cantilever Wings: A Mathematical Analysis, Checked by Experimental Tests, of the Free Oscillations in the System", Aircraft Engineering and Aerospace Technology, Vol. 7 No. 11, pp. 282-294. https://doi.org/10.1108/eb029987

Publisher

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MCB UP Ltd

Copyright © 1935, MCB UP Limited