Airplane stress analysis
Description:
Report 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.
Date:
January 1918
Creator:
Zahm, A. F. & Crook, L. H.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department