Aerodynamic heating of a wing as determined from a free-flight rocket-model test to Mach number 3.64
Description:
From Introduction: "The primary purpose of the wing instrumentation was to obtain data for use in design of NACA research missiles; however, it is believed that the wing is representative of typical supersonic designs and that the data will be of general use and interest. Only the wing data are reported herein."
Date:
September 11, 1956
Creator:
Swanson, Andrew G. & Rumsey, Charles B.