NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Buckling of rotating beamsThe stability of a beam subjected to compressive centrifugal forces arising from steady rotation about an axis which does not pass through the clamped end of the beam is analyzed to determine the critical rotational speeds for buckling in the inplane and out-of-plane directions. The differential equations of motion are solved numerically using an integrating matrix method in combination with an eigenanalysis to determine the eigenvalues from which stability is assessed. The results clarify several differences which have been identified in the literature relating to the proper behavior of the critical rotational speed for buckling as the radius of rotation of the clamped end of the beam is reduced.
Document ID
19800035979
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
White, W. F., Jr.
(U.S. Army, Structures Laboratory, Hampton Va., United States)
Kvaternik, R. G.
(NASA Langley Research Center Hampton, Va., United States)
Kaza, K. R. V.
(NASA Lewis Research Center Cleveland; Toledo, University, Toledo, Ohio, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1979
Publication Information
Publication: International Journal of Mechanical Sciences
Volume: 21
Issue: 12, 1
Subject Category
Structural Mechanics
Accession Number
80A20149
Distribution Limits
Public
Copyright
Other

Available Downloads

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