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Preliminary results from fatigue tests with reference to operational statisticsSimple elements were subjected to repeated loads of variable ampliture, chosen in such a way that they may be regarded as approximations to the operational loads (gust and maneuver) experienced by an airplane. The effect of varying some parameters was investigated briefly. Some discussion is given of the question whether a design according to current (1938 German) requirements for static strength is adequate from the fatigue point of view, and existing requirements on fatigue strength are compared,
Document ID
19930093964
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gassner, E
Date Acquired
August 16, 2013
Publication Date
May 1, 1950
Report/Patent Number
NACA-TM-1266
Accession Number
93R23290
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STATISTICS - LOADS, GUST
AIRPLANES - STRENGTH
LOADS

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