Theory of aircraft structural models subject to aerodynamic heating and external loads

William J. O'Sullivan, Jr
naca-tn-4115
Sep 1957


The problem of investigating the simultaneous effects of transient aerodynamic heating and external loads on aircraft structures for the purpose of determining the ability of the structure to withstand flight to supersonic speeds is studied.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1957/naca-tn-4115.pdf