Development eliminates problems associated with prohibitive number of possible system modes for fluttering compressor or turbine blade row; existence and uniqueness of extremely simple system flutter modes are proved for blade rows consisting of identical blades equally spaced about common rotor.
System mode shapes in flutter of compressor blade rows
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 23 , n 1
1956
13 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
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