A method and apparatus for generating a flow of heated air in an airfoil model of an inlet of an aircraft engine. Heated air is sent into a duct system associated with the airfoil model of the inlet of the aircraft engine. The heated air is circulated within the airfoil model of the inlet of the aircraft engine using the duct system in a manner that simulates air flowing in the inlet of the aircraft engine.
Inlet icing protection simulation system
2015-09-15
Patent
Electronic Resource
English
DYNAMIC RESONANCE SYSTEM AND METHOD FOR ANTI-ICING AND DE-ICING OF INLET GRIDS
European Patent Office | 2017
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