Category: Strength and Thermal Conditions of Aircraft, chapter: Aviation and Rocket-Space Engineering | Engineering Journal: Science and Innovation

Design-theoretical and experimental determination of physical and mechanical properties of the composite materials for the light aircraft fuselage multilayer load-bearing elements

Published: 03.10.2024

Authors: Tun Lin Htet, Prosuntsov P.V.

Published in issue: #10(154)/2024

DOI: 10.18698/2308-6033-2024-10-2392

Category: Aviation and Rocket-Space Engineering | Chapter: Strength and Thermal Conditions of Aircraft

Determination of thickness of the smooth metal panels with limitations in stability and static strength at the postbuckling behaviour taking into account the membrane and bending stresses

Published: 03.06.2024

Authors: Mitrofanov O.V., Toropylina E.Yu.

Published in issue: #6(150)/2024

DOI: 10.18698/2308-6033-2024-6-2365

Category: Aviation and Rocket-Space Engineering | Chapter: Strength and Thermal Conditions of Aircraft

Analysis of the spacecraft protective structures resistance to high-speed impact of the orbital debris aluminum particles

Published: 30.03.2024

Authors: Kolpakov V.I., Fedorov S.V., Vinogradova E.P.

Published in issue: #3(147)/2024

DOI: 10.18698/2308-6033-2024-3-2344

Category: Aviation and Rocket-Space Engineering | Chapter: Design, Construction, Production, Testing, and Operation of Aircraft

Method for calculating axisymmetric oscillations of the shells of revolution with liquid according to the differential model

Published: 15.02.2024

Authors: Nguyen C.M., Shelevaya D.R., Krasnorutsky D.A.

Published in issue: #2(146)/2024

DOI: 10.18698/2308-6033-2024-2-2338

Category: Aviation and Rocket-Space Engineering | Chapter: Strength and Thermal Conditions of Aircraft

Deformation of the layered composite plates at low-speed contact with a rigid indenter

Published: 30.10.2023

Authors: Le Viet Tuan V.T.

Published in issue: #10(142)/2023

DOI: 10.18698/2308-6033-2023-10-2312

Category: Aviation and Rocket-Space Engineering | Chapter: Strength and Thermal Conditions of Aircraft

Design, development and approbation of the numerical technique in simulating the wing aeroelastic state based on the finite element and control volumes methods

Published: 20.07.2023

Authors: Gunchin V.K., Bolshikh A.A., Ustinov B.E.

Published in issue: #7(139)/2023

DOI: 10.18698/2308-6033-2023-7-2291

Category: Aviation and Rocket-Space Engineering | Chapter: Design, Construction, Production, Testing, and Operation of Aircraft

Simulation of the aircraft landing gear legs with the plastically deformable shock absorbers

Published: 23.06.2023

Authors: Sumerin A.A., Shcheglov G.A.

Published in issue: #6(138)/2023

DOI: 10.18698/2308-6033-2023-6-2284

Category: Aviation and Rocket-Space Engineering | Chapter: Strength and Thermal Conditions of Aircraft

Aircraft icing mechanism analysis methods

Published: 20.04.2023

Authors: Egorov A.V.

Published in issue: #4(136)/2023

DOI: 10.18698/2308-6033-2023-4-2266

Category: Aviation and Rocket-Space Engineering | Chapter: Design, Construction, Production, Testing, and Operation of Aircraft

Product thermal regime determination on the Moon surface taking into account the specular-diffuse reflection

Published: 15.12.2022

Authors: Borschev N.O., Deniskina A.R., Emelyanov A.Yu.

Published in issue: #12(132)/2022

DOI: 10.18698/2308-6033-2022-12-2236

Category: Aviation and Rocket-Space Engineering | Chapter: Design, Construction, Production, Testing, and Operation of Aircraft

On quantitative assessment of the ergonomic indicators of life support systems of the manned spacecraft

Published: 17.11.2022

Authors: Glebov I.V., Potemkin A.L., Glebova O.I.

Published in issue: #11(131)/2022

DOI: 10.18698/2308-6033-2022-11-2227

Category: Aviation and Rocket-Space Engineering | Chapter: Design, Construction, Production, Testing, and Operation of Aircraft