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Development of aeroelastic analysis methods for turborotors and propfans, including mistuningThe NASA Lewis aeroelastic research program is focused on unstalled and stalled flutter, forced response, and whirl flutter of turborotors and propfans. The objectives are to understand the physical phenomena of cascade flutter and response including blade mistuning.
Document ID
19880013860
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kaza, Krishna Rao V. (Army Aviation Systems Command Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Publication Information
Publication: NASA, Lewis Research Center, Lewis Structures Technology, 1988. Volume 1: Structural Dynamics
Subject Category
Structural Mechanics
Accession Number
88N23244
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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