The aircraft hydraulic system units and pipelines heat exchange parameters study

Автор: Nikolaev V.N.

Журнал: Siberian Aerospace Journal @vestnik-sibsau-en

Рубрика: Aviation and spacecraft engineering

Статья в выпуске: 1 vol.24, 2023 года.

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The paper offers a method of mathematical modelling of aircraft hydraulic system thermal state. The given mathematical model presents a system of partial differential equations for carbon-fiber composite thermal insulation together with ordinary differential equations for hydraulic system components that describe their heat exchange with the ambient air and close-located surfaces. To solve the direct thermal state problem for hydraulic system components, i. e., to solve a stiff ordinary differential equation system, a Rosenbrock-type second order approximation numerical scheme for non-autonomous systems was applied. A solution of a partial differential equation system in Monte-Carlo method based on a probabilistic representation of the solution as a functional expectation of the diffusion process was also used. The inverse problem of the hydraulic system elements’ thermal state was solved applying a composition of the steepest descent method, Newton method and quasi-Newton method of Broydon-Fletcher-Goldfarb-Shanno. A mathematical model of the thermal state of a hydraulic system unit operating in an unpressurized aircraft compartment has been also developed, and the confidence intervals of each of the required model coefficients have been estimated using 2 1 α χ distribution at confidence probability = 0.95.

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Mathematical model, differential equations, aircraft hydraulic system, parametric identification, confidence intervals of model coefficients

Короткий адрес: https://sciup.org/148329681

IDR: 148329681   |   DOI: 10.31772/2712-8970-2023-24-1-136-143

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