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FACTORS IN EVALUATING FATIGUE LIFE ON STRUCTURAL PARTSVariable amplitude loading, fatigue loading, fatigue crack propagation and structural parts - fatigue life
Document ID
19630004832
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Illg, W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1960
Subject Category
Thermodynamics And Combustion
Accession Number
63N14708
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VTOL AIRCRAFT
FATIGUE TEST
FATIGUE
CRACK PROPAGATION

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IDRelationTitle19630004807Collected WorksConference on V/Stol Aircraft a Compilation of the Papers Presented at Langley Research Center, Langley Field, VA., Nov. 17-18, 1960
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