Description: Report presenting the application of transient theory to the rational determination of dynamic loads on airplane structures during initial landing impact. Simplified procedures are described by which the distribution of the maximum attainable value of the dynamic stresses in the structure may be obtained.
Date: October 1944
Creator: Biot, M. A. & Bisplinghoff, R. L.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department