Zobrazeno 1 - 10
of 14
pro vyhledávání: '"A. N. Klyuchnikov"'
Publikováno v:
AIP Conference Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ccc555b0690773260e4e3b78a88a1b7b
https://doi.org/10.1063/1.5044144
https://doi.org/10.1063/1.5044144
Autor:
S. N. Klyuchnikov, V. L. Zemlyakov
Publikováno v:
Measurement Techniques. 55:1214-1218
A new method of determining the Q-factor of piezo resonators from measurements at only a single frequency is proposed. The method is implemented in a device without memory elements and makes it possible to automatically generate an electrical signal
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a9ffba141e22177d1539049c0188f64c
https://doi.org/10.1007/s11018-012-0110-0
https://doi.org/10.1007/s11018-012-0110-0
Publikováno v:
Combustion, Explosion, and Shock Waves. 48:177-190
A single mechanism for the combustion of mixtures of binders capable of self-sustained combustion with inert or active fillers is proposed. A mathematical model for the combustion of such mixtures is developed which takes into account the curvature o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5151523e6f56f4fbccde0491c984f514
https://doi.org/10.1134/s0010508212020074
https://doi.org/10.1134/s0010508212020074
Publikováno v:
Combustion, Explosion, and Shock Waves. 48:33-40
A software system is developed for solving an adjoint problem for modeling intrachamber processes of an axisymmetric solid-propellant charge attached to the casing. This system predicts intraballistic, strength, and gas-dynamic characteristics of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aec3496a6d369cba3abf394905472d45
https://doi.org/10.1134/s0010508212010054
https://doi.org/10.1134/s0010508212010054
Publikováno v:
Combustion, Explosion, and Shock Waves. 46:593-598
A methodical approach to evaluating the loss in rocket motor specific impulse due to discontinuity of the contour of the supersonic part of the nozzle block is developed based on calculating the parameters of the nonisentropic flow of combustion prod
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f9d7b00c0a3c35677aaed741a0d967a2
https://doi.org/10.1007/s10573-010-0078-5
https://doi.org/10.1007/s10573-010-0078-5
Autor:
V. L. Zemlyakov, S. N. Klyuchnikov
Publikováno v:
Measurement Techniques. 53:301-304
A new method of measuring the parameters of a piezoceramic element is proposed, the basis of which is the maximum values of the amplitudes of the conductance and its derivative. The method only requires simple automated instruments.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::857153aa4dfc3a49b0547de8ce6488ec
https://doi.org/10.1007/s11018-010-9500-3
https://doi.org/10.1007/s11018-010-9500-3
Autor:
G. B. Manelis, V. A. Strunin, S. V. Gunin, A. N. Klyuchnikov, A. V. Fedorychev, Yu. M. Milekhin
Publikováno v:
Combustion, Explosion, and Shock Waves. 46:315-324
A mathematical model for combustion of a propellant with a coolant taking into account the two-zone structure of the combustion front due to condensed- and gas-phase reactions was developed and examined. Formulas for the burning rate, reaction-zone t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c9ad317f462ad35db8b42199adea85ec
https://doi.org/10.1007/s10573-010-0044-2
https://doi.org/10.1007/s10573-010-0044-2
Publikováno v:
Doklady Physical Chemistry. 432:96-100
96 The velocity of combustion of condensed energy� rich systems in a pilot engine unit generally exceeds the combustion velocity in a laboratory constantpres� sure setup. This is caused by differences in heat trans� fer between the burning prop
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::96b433387ed39697c558fcd69d392550
https://doi.org/10.1134/s0012501610050039
https://doi.org/10.1134/s0012501610050039
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 9:233-247
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::649be6e84a3de1719c13777edad047a5
https://doi.org/10.1615/intjenergeticmaterialschemprop.v9.i3.40
https://doi.org/10.1615/intjenergeticmaterialschemprop.v9.i3.40
Publikováno v:
Combustion, Explosion, and Shock Waves. 45:678-685
Existing concepts of the effect of tensile strains on the burning rate of propellants are analyzed. It is demonstrated that the basic mechanism of increasing burning rate of composite propellants under tension is spalling of the binder from oxidizer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::120c64d7e468b31eb02768d044f298c0
https://doi.org/10.1007/s10573-009-0084-7
https://doi.org/10.1007/s10573-009-0084-7