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Reduction of wind-tunnel-model vibration by means of a tuned damped vibration absorber installed in the model

Author
Igoe, W. B.
Published
Jul 1, 1968.
Physical Description
1 electronic document
Additional Creators
Capone, F. J.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Wind tunnel model vibration reduced by use of tuned vibration damping absorber on aircraft model
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19680019334.
Accession ID: 68N28806.
NASA-TM-X-1606.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15954950