Matrix equations governing transverse vibration of rotating twisted cantilever beam, such as airplane propeller or turbine blade, are developed; from these equations variation in natural frequency with rotational speed may be found, and some simplified methods for finding these curves are shown. See also Engineering Index 1949 p 44, under Airplane Propellers -- Stresses.
Free and forced vibrations of rotating blades
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 18 , n 4
1951
5 pages
Article (Journal)
English
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On the free transverse vibrations of airscrew blades
SLUB | 1922
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