NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
An improved method to determine vibration damping of materials and structural componentsThe present, improved frequency-domain technique for vibration-damping estimation involves the fitting of a 'best curve' for the measured frequency-response data near a resonance by means of a least-squares error criterion. The damping ratio and the undamped natural frequency are then computed using the coefficients of the rational fraction polynomial that had been determined on the basis of the curve-fitting technique. Attention is given to the results of this method's application to damping measurements for graphite-reinforced epoxy composites. The results obtained are superior to those of the 'half-power points' method.
Document ID
19920063310
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rao, Mohan D.
(Michigan Technological University Houghton, United States)
Crocker, Malcolm J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Zhu, G. H.
(Auburn University AL, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Subject Category
Structural Mechanics
Meeting Information
Meeting: International Congress on Recent Developments in Air and Structure-Borne Sound and Vibration
Location: Auburn, AL
Country: United States
Start Date: March 6, 1990
End Date: March 8, 1990
Accession Number
92A45934
Funding Number(s)
CONTRACT_GRANT: NAS8-36146
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available