Abstract

A brief presentation is made of some of the radiant-heating apparatus developed by the National Advisory Committee for Aeronautics (NACA) to simulate aerodynamic heating of aircraft structures. Some results of the effects of thermal stresses on the stiffness and deflection of aircraft structures are demonstrated by tests incorporating the radiant-heating apparatus.

Issue Section:
Research Papers
Topics:
Aircraft, Transient heat transfer, Radiant heating, Aeronautics, Deflection, Heating, Stiffness, Thermal stresses
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