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Fittings and Other Structural Parts of AirplanesThe strength and reliability of airplanes depend greatly on the careful design and manufacture of fittings, couplings, and other highly stressed parts. The more important parts of the airplane must be occasionally tested for increased loads and in order to avoid the possibility of defects creeping in during subsequent production. Strength tests are discussed for fittings for wing spar joints, fittings for strut connections, internal bracing, control gear, and landing gear.
Document ID
19930080944
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Eydam, P
Date Acquired
September 6, 2013
Publication Date
October 1, 1923
Report/Patent Number
NACA-TN-160
Report Number: NACA-TN-160
Accession Number
93R10234
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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