NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A new approach to the explanation of the flutter mechanismStructural stability of bending torsion flutter model
Document ID
19660006195
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Rheinfurth, M. H.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Swift, F. W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-3125
Report Number: NASA-TN-D-3125
Accession Number
66N15484
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STRUCTURAL STABILITY
BENDING
MATHEMATICAL MODEL
FLUTTER
TORSION
No Preview Available