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Fatigue Strength of Airplane and Engine MaterialsThis report was undertaken to give a brief summary of the laws governing the fatigue stresses and of the most important strength coefficients necessary for the correct dimensioning of the structural members.
Document ID
19930094674
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Matthaes, Kurt
Date Acquired
September 6, 2013
Publication Date
April 1, 1934
Report/Patent Number
NACA-TM-743
Accession Number
93R23594
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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