Areas of research


The technologies include theoretical models, numerical algorithms, software platforms, and experimental approaches that will allow the team to establish fundamental physical principles for:

Prospective spacecraft aerothermodynamics


Mach number flowfield around the prospective spacecraft "Clipper" and distribution of the heat transfer coefficient on its surface.

Conventional and advanced propulsion technologies

Micronozzle start

Starting process in micronozzle, numerical simulation based on model kinetic equations.

Gaseous and multiphase flows in MEMS


Instability and transition to turbulence in compressible hypersonic flows


Instability of boundary layer on the flat plate at M = 6, isosurfaces of vorticity (Q-criterion).