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Development of aeroelastic analysis methods for turborotors and propfans, including mistuning

Author
Kaza, Krishna Rao V.
Published
May 1, 1988.
Physical Description
1 electronic document
Online Version

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
The 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.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19880013860.
Accession ID: 88N23244.
NASA, Lewis Research Center, Lewis Structures Technology, 1988. Volume 1: Structural Dynamics; p 247-262.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15694791