NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Application of Zimmerman flutter-margin criterion to a wind tunnel modelThe Zimmerman flutter margin criterion was studied by applying it to data obtained from a wind tunnel model. The sensitivity of the flutter margin parameter was explored with a parametric trend study and by calculation of the derivatives with respect to the input frequency and damping parameters. The criterion is simple in concept and application, and it serves as a good flutter onset predictor because it gives a nearly linear variation with dynamic pressure. However, accurate values of both frequency and damping of both modes involved in flutter are required for reliable flutter onset prediction. The simplified version using only frequencies gave a highly nonconservative flutter onset in one case and should not be used in general.
Document ID
19830003800
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bennett, R. M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1982
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-84545
L-15508
NAS 1.15:84545
Report Number: NASA-TM-84545
Report Number: L-15508
Report Number: NAS 1.15:84545
Accession Number
83N12070
Funding Number(s)
PROJECT: RTOP 505-33-53-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available