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    An Assessment of Technology for Turbojet Engine Rotor Failures (1977)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: Design 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.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-CP-2017 , E-8305 , Mar 29, 1977 - Mar 31, 1977; Cambridge, MA; United States
    Format: application/pdf
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