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A numerical method for determining the natural vibration characteristics of rotating nonuniform cantilever bladesA method is presented for determining the free vibration characteristics of a rotating blade having nonuniform spanwise properties and cantilever boundary conditions. The equations which govern the coupled flapwise, chordwise, and torsional motion of such a blade are solved using an integrating matrix method. By expressing the equations of motion and matrix notation, utilizing the integrating matrix as an operator, and applying the boundary conditions, the equations are formulated into an eigenvalue problem whose solutions may be determined by conventional methods. Computer results are compared with experimental data.
Document ID
19760003417
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
White, W. F., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Malatino, R. E.
(Naval Air Systems Command)
Date Acquired
September 3, 2013
Publication Date
October 1, 1975
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-72751
Report Number: NASA-TM-X-72751
Accession Number
76N10505
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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