Semi‐Cantilever Wings: A Mathematical Analysis, Checked by Experimental Tests, of the Free Oscillations in the System
Aircraft Engineering and Aerospace Technology
Article publication date: 1 November 1935
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.
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
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