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Analysis of simple 2-D and 3-D metal structures subjected to fragment impactTheoretical methods were developed for predicting the large-deflection elastic-plastic transient structural responses of metal containment or deflector (C/D) structures to cope with rotor burst fragment impact attack. For two-dimensional C/D structures both, finite element and finite difference analysis methods were employed to analyze structural response produced by either prescribed transient loads or fragment impact. For the latter category, two time-wise step-by-step analysis procedures were devised to predict the structural responses resulting from a succession of fragment impacts: the collision force method (CFM) which utilizes an approximate prediction of the force applied to the attacked structure during fragment impact, and the collision imparted velocity method (CIVM) in which the impact-induced velocity increment acquired by a region of the impacted structure near the impact point is computed. The merits and limitations of these approaches are discussed. For the analysis of 3-d responses of C/D structures, only the CIVM approach was investigated.
Document ID
19780002135
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Witmer, E. A.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Stagliano, T. R.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Spilker, R. L.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Rodal, J. J. A.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1977
Publication Information
Publication: Assessment of Technol. for Turbojet Engine Rotor Failures
Subject Category
Aircraft Propulsion And Power
Accession Number
78N10078
Funding Number(s)
CONTRACT_GRANT: NGR-22-009-339
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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