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An Assessment of Technology for Turbojet Engine Rotor FailuresDesign considerations, objectives, and approaches used in containing rotor burst debris are discussed. Methods are given for determining the fracture resistance of various materials used in providing lightweight shielding from fragment impact.
Document ID
19780002125
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Witmer, E. A. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CP-2017
E-8305
Report Number: NASA-CP-2017
Report Number: E-8305
Accession Number
78N10068
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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