 | | Mechanics of Solids
A Journal of Russian Academy of Sciences | | Founded
in January 1966
Issued 6 times a year
Print ISSN 0025-6544
Online ISSN 1934-7936 |
Archive of Issues
| Total articles in the database: | | 12804 |
| In Russian (Èçâ. ÐÀÍ. ÌÒÒ): | | 8044
|
| In English (Mech. Solids): | | 4760 |
|
| << Previous article | Volume 56, Issue 1 / 2021 | Next article >> |
| Ovchinnikov V.V. and Petrov Yu.V., "Investigation of the Influence of Elastic Dissipative Parameters of the Under Wing Pylon-Mounted Engine Suspension on Aeroelastic and Strength Characteristics of the Aircraft," Mech. Solids. 56 (1), 95-102 (2021) |
| Year |
2021 |
Volume |
56 |
Number |
1 |
Pages |
95-102 |
| DOI |
10.3103/S0025654421010106 |
| Title |
Investigation of the Influence of Elastic Dissipative Parameters of the Under Wing Pylon-Mounted Engine Suspension on Aeroelastic and Strength Characteristics of the Aircraft |
| Author(s) |
Ovchinnikov V.V. (Bauman Moscow State Technical University, Moscow, 105005, Russia)
Petrov Yu.V. (Moscow State Technical University of Civil Aviation, Moscow, 125993, Russia, doctor561@rambler.ru) |
| Abstract |
To study the influence and selection of rational elastic-dissipative parameters for under wing pylon-mounted engine suspension, a mathematical model of aeroelasticity of a large-sized transport aircraft has been developed by taking into account the kinetic moment of the engine rotors and specially designed engine attachment points to the pylons. It is shown that the elastic-dissipative parameters of the attachment points, which implement the concept of a released engine, have a significant effect on the integral aeroelastic and strength characteristics of the aircraft. Schematic diagrams of the engine mounts to the pylon are proposed. The usefulness of the concept of a released engine for increasing aeroelastic stability and reduce the level of fatigue damage of the aircraft structural elements has been proved. |
| Keywords |
aeroelasticity, pylon-mounted engine, elastic-dissipative constraints, aeroelastic stability, fatigue damage |
| Received |
22 September 2019 | Revised |
15 October 2020 | Accepted |
25 October 2020 |
| Link to Fulltext |
|
| << Previous article | Volume 56, Issue 1 / 2021 | Next article >> |
|
 If you find a misprint on a webpage, please help us correct it promptly - just highlight and press Ctrl+Enter
|
|
Russian 
English