Theoretical and experimental investigation of the photographic reconnaissance plane instrument bay thermal state

Abstract


A mathematical model of the venting heat-insulated instrument bay of the photographic reconnaissance plane thermal state is developed. Direct and inverse problems of heat exchange are solved, confidence intervals of estimated parameters are determined.


About the authors

V. N. Nikolayev

Federal State Unitary Enterprise "S. A. Chaplygin Siberian Aeronautical Research Institute"

Author for correspondence.
Email: nikvla50@mail.ru

Russian Federation

candidate of technical sciences
head of a sector

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