As of 19.05.2020
Name of the project: Research and development of physical models and quantitative technologies of description of combustion modes in engines of aircraft
Strategy for Scientific and Technological Development Priority Level: а, б
Research directions:
- Modernisation, development and highly efficient software implementation of physical models of high-speed turbulent combustion in channels oriented towards computations within the RANS and LES approaches.
-
A Russian database of experiments in high-speed flows with combustion in channels has been created on the basis of the «fire» aerodynamic experiment (conducted in the ADT T-131 wind tunnel of the Central Aerohydrodynamic Institute – TsAGI).
- Development and detailed quantitative and theoretical research of the model of engines with a resonator cavity in which combustion of fuel occurs in a rotating detonation wave.
Project objective:
Development and validation of models of various modes of combustion in jet engines as well as creation of specialised software for a cycle of aerodynamic design processes to build aircraft engines.
Hosting organization
|
Field of studies
|
City
|
Invited researcher
|
Time span of the project
|
---|---|---|---|---|
Laboratory of Self-healing Construction Materials
Peter the Great St.Petersburg Polytechnic University |
Mechanics and machinery |
St. Petersburg |
Kordas Georgios
Greece |
2021-2023 |
Research Laboratory for the Mechanics of Bio-compatible Materials and Devices
Perm National Research Polytechnic University |
Mechanics and machinery |
Perm |
Silberschmidt Vadim
United Kingdom |
2021-2023 |
Laboratory of Digitalisation, Analysis and Synthesis of Complex Mechanical Systems, Networks and Environments
Institute for Problems in Mechanical Engineering of the Russian Academu of Sciences |
Mechanics and machinery |
St. Petersburg |
Fridman Emilia Moiseevna
Israel |
2021-2023 |