Development of a Numerical Model Designed to Calculate the Temperature Field and Thermal Stresses in Structural Elements of Aircrafts

The algorithm for the numerical solution of the quasistatic thermoelasticity problem in the domains of simple spatial forms is briefly described. The initial validation and verification of the developed numerical technique was performed. Some results of the solution of the quasistatic thermoelastici...

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Veröffentlicht in:	Fluid dynamics 2022-12, Vol.57 (Suppl 1), p.S170-S180
Hauptverfasser:	Kuzenov, V. V., Shumaev, V. V., Dobrynina, A. O.
Format:	Artikel
Sprache:	eng
Schlagworte:	Algorithms Classical and Continuum Physics Classical Mechanics Engineering Fluid Dynamics Fluid- and Aerodynamics Numerical models Physics Physics and Astronomy Structural members Temperature distribution Thermal stress Thermoelasticity
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Zusammenfassung:	The algorithm for the numerical solution of the quasistatic thermoelasticity problem in the domains of simple spatial forms is briefly described. The initial validation and verification of the developed numerical technique was performed. Some results of the solution of the quasistatic thermoelasticity problem in the simplest structural elements of aircraft.
ISSN:	0015-4628 1573-8507
DOI:	10.1134/S0015462822601425