The quantitative effect of a flexible fuselage on the symmetric torsional modes of the wings of a large airplane
Using Holzer's method of frequency calculation, the natural frequencies for the first two modes of torsional vibration of the wing were determined for a representative conventional airplane (B24-C) in the customary manner, the fuselage being considered as a rigid body. Next, using a method deve...
Internet
https://thesis.library.caltech.edu/6409/1/Furer_ab_1944.pdfDunn, William C. and Furer, Albert B. (1944) The quantitative effect of a flexible fuselage on the symmetric torsional modes of the wings of a large airplane. Engineer's thesis, California Institute of Technology. doi:10.7907/H4PK-H195. https://resolver.caltech.edu/CaltechTHESIS:05192011-093121243 <https://resolver.caltech.edu/CaltechTHESIS:05192011-093121243>