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Approximate analysis of containment/deflection ring responses to engine rotor fragment impact.The transient responses of containment and/or deflection rings to impact from an engine rotor-blade fragment are analyzed. Energy and momentum considerations are employed in an approximate analysis to predict the collision-induced velocities which are imparted to the fragment and to the affected ring segment. This collision analysis is combined with the spatial finite-element representation of the ring and a temporal finite-difference solution procedure to predict the resulting large transient elastic-plastic deformations of containment/deflection rings. Some comparisons with experimental data are given.
Document ID
19730034386
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Wu, R. W.-H.
Witmer, E. A.
(MIT Cambridge, Mass., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Publication Information
Publication: Journal of Aircraft
Volume: 10
Subject Category
Structural Mechanics
Accession Number
73A19188
Funding Number(s)
CONTRACT_GRANT: NGR-22-009-339
Distribution Limits
Public
Copyright
Other

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