Measurement Technology and Metrology
Аuthors
Abstract
The mathematical model of the thermal state of the bay is developed. The direct and inverse problems of heat exchange are solved. The confidence intervals of estimated parameters are determined. The values of temperature and air consumption in the thermal conditions supporting system in the venting heat-insulated instrument bay of the photographic reconnaissance plane are obtained.Keywords:
mathematical model, direct problem, inverse problem, thermal state, airborne equipment, thermal conditions supporting system, instrument bay.
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