Анализ влияния постоянных управляющих воздействий на область значений функционалов гиперзвуковой аэродинамики
DOI:
https://doi.org/10.17308/sait.2018.2/1204Keywords:
control, heat and mass transfer, laminar boundary layer, hypersonic flows, permeable surfaces, total heat flow, total Newton friction force, method of generalized integral relations, approximating system of ordinary differential equations, nonlinear algebraic equations systemAbstract
The properties of mathematical model of heat and mass transfer and friction control in laminar boundary layer on permeable cylindrical and spherical surfaces of hypersonic aircraft are investigated. The dependences of hypersonic aerodynamics functionals (the total heat flow and the total Newton friction force) values on controls (the blowing into boundary layer, the temperature factor, the magnetic field) are obtained. The computational experiments results are presented.
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