Zobrazeno 1 - 10
of 41
pro vyhledávání: '"B. V. Smorodsky"'
Publikováno v:
SIBERIAN JOURNAL OF PHYSICS. 17:41-47
A study of the effect of distributed gas with high specific heat capacity blowing into the supersonic boundary layer on its stability to artificial disturbances was conducted. It is shown that the injection of gas with high heat capacity Cp at certai
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Autor:
B. V. Smorodsky, S. A. Gaponov
Publikováno v:
Thermophysics and Aeromechanics. 27:205-217
The paper presents a theoretical study for a supersonic boundary layer over a flat plate in a stream of air at Mach number M = 2 under the conditions of surface sublimation. The sublimation-prone material is naphthalene (C10H8). Calculations demonstr
Publikováno v:
Thermophysics and Aeromechanics. 27:81-88
A method of direct numerical simulation and a method of solving the boundary-layer equations were applied to parameters of a supersonic boundary layer for a flow past a flat plate (Mach number M = 2) for the case of a plate coated with a sublimation
Autor:
Aleksey A. Yatskikh, Alexander D. Kosinov, N. V. Semionov, G. L. Kolosov, Yury G. Yermolaev, B. V. Smorodsky, Alexander N. Semenov
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 234:96-101
The paper is devoted to an experimental and theoretical study of effect of moderate angle-of-attack variation on disturbances evolution and laminar-turbulent transition in a supersonic boundary layer on swept wing at Mach 2. Monotonous growth of the
Autor:
B. V. Smorodsky, S. A. Gaponov
Publikováno v:
Siberian Journal of Physics. 14:25-39
Publikováno v:
Siberian Journal of Physics. 14:26-38
Experimental investigation of the influence of the distributed heavy gas (sulfur hexafluoride, SF6) injection into the near-wall sub-layer of a boundary layer) on the hydrodynamic stability in relation to controlled disturbances of the supersonic fla
Publikováno v:
AIP Conference Proceedings.
The theoretical and experimental investigation of the effect of the heavy gas (sulfur hexafluoride) blowing into the boundary layer on the hydrodynamic stability to controlled perturbations of the supersonic flat-plate boundary layer at Mach number 2
Publikováno v:
AIP Conference Proceedings.
The paper presents results of a theoretical study on the properties of a supersonic boundary layer and its linear stability under conditions of surface material sublimation. Calculations were performed for an adiabatic-wall boundary layer over a camp
Publikováno v:
Thermophysics and Aeromechanics. 25:183-190
Experiments were performed on the influence of distributed injection of a heavy gas (elegas SF6) into the near-wall region of the supersonic (freestream Mach number М∞ = 2) boundary layer on its stability in relation to natural disturbances. Heavy