Work

Development of a numerical model designed to calculate the temperature field and thermal stresses in structural elements of aircrafts

Year: 2019

Type: article

Abstract: 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.

Source: Physical-Chemical Kinetics in Gas Dynamics

DOI: 10.33257/phchgd.19.4.757

Authors: V.V. Kuzenov, V.V. Shumaev, A.O. Dobrynina

Institutions: Bauman Moscow State Technical University, All Russia Research Institute of Automatics

Language: English

Topic: Thermoelastic and Magnetoelastic Phenomena

Subfield: Mechanics of Materials

Field: Engineering

Domain: Physical Sciences

Open Access status: diamond

OpenAlex ID: W2942190825

FWCI:

Cites: 7

Cited by:

Related to: 10