Zobrazeno 1 - 10
of 47
pro vyhledávání: '"A. K. Tretyakov"'
Autor:
P. K. Tretyakov, A. V. Tupikin
Publikováno v:
Combustion, Explosion, and Shock Waves. 58:531-535
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Kerosene Combustion in a Pseudoshock with Varied Conditions at the Supersonic Ramjet Combustor Model
Publikováno v:
Combustion, Explosion, and Shock Waves. 57:635-639
Autor:
O. V. Egorov, A. K. Tretyakov
Publikováno v:
Russian Physics Journal. 64:1363-1372
Publikováno v:
Физика горения и взрыва. 57:3-7
Autor:
A. A. Savarovskii, P. K. Tretyakov, A. V. Tupikin, A. L. Kuranov, S. V. Kolosenok, V. M. Abashev
Publikováno v:
Combustion, Explosion, and Shock Waves. 56:533-536
This study experimentally confirms the intensification of kerosene combustion in the case where a mixture simulating steam reformation products in a model combustion chamber with a supersonic velocity of the flow at the inlet. It is shown that the us
Autor:
A. K. Tretyakov, O. V. Egorov
Publikováno v:
Russian Physics Journal. 63:607-615
The interaction energy of the ozone molecule with atoms of noble gases (Ar and He) is analyzed. The coupled cluster methods CCSD(T) and CCSD(T)-F12 with orbital basis sets including electrons from diffuse orbitals (aug-cc-pVXZ for X = D, T, Q, 5, …
Autor:
P. K. Tretyakov
Publikováno v:
Combustion, Explosion, and Shock Waves. 56:36-40
A new method of initiation and effective burning of kerosene at supersonic velocities of the flow in a constant-section channel is considered as applied to combustion chambers of variable geometry. The regime of intense combustion occurs due to an ex
Autor:
P. K. Tretyakov
Publikováno v:
Доклады Академии наук. 489:250-253
A technique has been proposed and the possibility of its realization for the initiation of kerosene combustion in supersonic air flow in part of the combustion chamber (CC) of a constant cross section has been confirmed. The intense combustion regime
Autor:
P. K. Tretyakov
Publikováno v:
Doklady Physics. 64:438-441
In this paper, we propose a method to initiate combustion of kerosene in a supersonic air flow in part of a combustion chamber with a constant cross section and experimentally confirm the possibility of its implementation. An intensive combustion mod