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Airplane Stress AnalysisReport presents stress analysis of individual components of an airplane. Normal and abnormal loads, sudden loads, simple stresses, indirect simple stresses, resultant unit stress, repetitive and equivalent stress, maximum steady load and stress are considered.
Document ID
19930091143
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Report
Authors
Zahm, A F
Crook, L H
Date Acquired
September 6, 2013
Publication Date
January 1, 1918
Report/Patent Number
NACA-TR-82
Report Number: NACA-TR-82
Accession Number
93R20433
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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