Modelling Combined Heat Exchange in the Leading Edge of Perspective Aircraft Wing

Kandinsky, Roman O.; Prosuntsov, P. V.

doi:10.1051/matecconf/20152301019

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Navier-stokes System and Equations Of Chemical Kinetics1

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2023

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Cited by 5 publications

(2 citation statements)

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“…To solve the gas dynamics system the finite volume method is used and for the heat and mass transfer system the finite element method is used [11,13].…”

Section: Methodsmentioning

confidence: 99%

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Finite element modeling of thermal stresses in aerospace structures from polymer composite materials

Dimitrienko

Koryakov²,

Yurin³

et al. 2023

E3S Web of Conf.

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The conjugate problem of aerodynamics and heat and mass transfer in heat-shielding structures made of ablating polymer composite materials is considered. To determine the heat fluxes in the shock layer, the chemical composition of the atmosphere is taken into account. A mathematical formulation of the joint problem is formulated and an algorithm for numerical solution is proposed. An example of a numerical solution of the problem for the reentry spacecraft Stardust is presented. It is shown that due to the high temperatures of aerodynamic heating of a structure made of a polymer composite material, an intense internal generation of gas appears in the structure of the material, which can lead to the destruction of the material.

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“…To solve the gas dynamics system the finite volume method is used and for the heat and mass transfer system the finite element method is used [11,13].…”

Section: Methodsmentioning

confidence: 99%

“…Consider the system of equations for a viscous, chemically-reacting heat-conducting gas [8][9][10][11][12][13][14][15][16]:…”

Section: Navier-stokes System and Equations Of Chemical Kineticsmentioning

confidence: 99%

Finite element modeling of thermal stresses in aerospace structures from polymer composite materials

Dimitrienko

Koryakov²,

Yurin³

et al. 2023

E3S Web of Conf.

View full text Add to dashboard Cite

show abstract

Wing airfoil selection and optimization for the tourist class reusable space vehicle

Ashikhmina

Prosuntsov

2019

International Youth Scientific Conference “Heat and Mass Transfer in the Thermal Control System of Technical and Technological

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Modelling the heating and ablation of carbon-ceramic composite materials of various density

Barinov

Prosuntsov

2019

International Youth Scientific Conference “Heat and Mass Transfer in the Thermal Control System of Technical and Technological

View full text Add to dashboard Cite

Modelling Combined Heat Exchange in the Leading Edge of Perspective Aircraft Wing

Cited by 5 publications

References 6 publications

Finite element modeling of thermal stresses in aerospace structures from polymer composite materials

Finite element modeling of thermal stresses in aerospace structures from polymer composite materials

Wing airfoil selection and optimization for the tourist class reusable space vehicle

Modelling the heating and ablation of carbon-ceramic composite materials of various density

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