FIELD: test equipment.
SUBSTANCE: invention relates to aircraft engineering, particularly, to methods of reproducing aerodynamic heat and power effects on aircraft inner surface in ground conditions. Proposed device comprises housing with housing arranged inside said housing. Housing is made in the form of a row of isolated from each other, equidistant inner surface of the compartment of the aircraft compartment. Heaters are quartz halogen lamps fixed on each section at equal distance from each other and with a gap relative to inner surface of compartment of aircraft. Each section contains aluminum disks for reflection and accumulation of heat. On the base of the stand there installed are nozzles for supply and depressurisation.
EFFECT: technical result consists in ensuring best matching of distribution of heat flux, high efficiency and accuracy of measurement results of heat resistance of materials.
1 cl, 1 dwg
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