Zobrazeno 1 - 10
of 122
pro vyhledávání: '"V. S. Aksenov"'
Autor:
V. S. Ivanov, S. M. Frolov, V. S. Aksenov, F. S. Frolov, Igor O. Shamshin, I. A. Sadykov, R. R. Tukhvatullina, A. E. Zangiev, S. V. Platonov, K. A. Avdeev
Publikováno v:
Shock Waves. 32:11-24
The physical and mathematical model for simulating combustion and detonation of fuel mixture in the semi-confined gas volumes above the free surface of water is applied for modeling the transient two-phase reactive flow in the gas cavity under the bo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1c315f814fd269f820689e90c73e46fc
https://doi.org/10.1007/s00193-021-01046-2
https://doi.org/10.1007/s00193-021-01046-2
Autor:
Igor O. Shamshin, F. S. Frolov, V. S. Aksenov, I. A. Sadykov, R. R. Tukhvatullina, A. E. Zangiev, S. V. Platonov, K. A. Avdeev, S. M. Frolov, V. S. Ivanov
Publikováno v:
Shock Waves. 32:1-10
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::28e83ce0855a4ac7e49a744bdd658690
https://doi.org/10.1007/s00193-021-01045-3
https://doi.org/10.1007/s00193-021-01045-3
Publikováno v:
Combustion Science and Technology. 194:3432-3466
Deflagration-to-detonation transition (DDT) in gas (oxygen)–liquid n-heptane film and gas (oxygen)–liquid n-decane film systems is registered experimentally using a fused or exploding wire as a wea...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::74c3923f72662b6baa9ae68edcee9ef9
https://doi.org/10.1080/00102202.2021.1929196
https://doi.org/10.1080/00102202.2021.1929196
Autor:
V. S. Aksenov, P. A. Gusev, Igor O. Shamshin, I. V. Bilera, V. I. Zvegintsev, M. V. Kazachenko, M. S. Belotserkovskaya, S. M. Frolov
Publikováno v:
Shock Waves. 30:721-739
A new experimental method for evaluating the detonability of fuel–air mixtures (FAMs) based on measuring the deflagration-to-detonation (DDT) run-up distance and/or time in a standard pulse detonation tube (SDT) is used to rank gaseous premixed and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a16b34590e48143db69881bead5507c3
https://doi.org/10.1007/s00193-020-00966-9
https://doi.org/10.1007/s00193-020-00966-9
Autor:
D. V. Igonkin, E. Yu. Marchukov, A. A. Illarionov, S. M. Frolov, I. V. Mokrynskij, Igor O. Shamshin, V. S. Ivanov, M. Yu. Vovk, V. S. Aksenov, S. N. Moskvitin, V. A. Bruskov
Publikováno v:
Doklady Physics. 65:36-39
For the first time, a detonation afterburner (DA) for continuous detonation combustion of TS-1 aviation kerosene was developed, manufactured, and tested. Test fires of the DA in combination with a TJ100S-125 small-sized single-circuit turbojet engine
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1367635157906abcce26f7cc1d7ce8b4
https://doi.org/10.1134/s1028335820010061
https://doi.org/10.1134/s1028335820010061
Autor:
S. M. Frolov, V. I. Zvegintsev, V. S. Aksenov, I. V. Bilera, M. V. Kazachenko, I. O. Shamshin, P. A. Gusev, M. S. Belotserkovskaya
Publikováno v:
Доклады Академии наук. 488:162-166
A new method for determining the detonability of fuel is proposed based on the measured values of the detonation run-up distance and time in the standard pulsed detonation tube (PDT). Granulated polypropylene (GP) was used as a fuel. A test ben
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5064240ace59878cb88842d77677626e
https://doi.org/10.31857/s0869-56524882162-166
https://doi.org/10.31857/s0869-56524882162-166
Autor:
V. S. Aksenov, S. M. Frolov, V. I. Zvegintsev, Igor O. Shamshin, I. V. Bilera, V. M. Kazachenko, P. A. Gusev, M. S. Belotserkovskaya
Publikováno v:
Doklady Physical Chemistry. 488:129-133
A new method to determine fuel detonability has been proposed, which is based on measuring the length and time of a deflagration-to-detonation transition (DDT) in a calibration pulsed-detonation wind tunnel (CPDWT). The fuel was polypropylene granule
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8b7aec6d8111a9f05090560c962747ef
https://doi.org/10.1134/s0012501619090045
https://doi.org/10.1134/s0012501619090045
Autor:
F. S. Frolov, R. R. Tukhvatullina, S. M. Frolov, K. A. Avdeev, V. S. Aksenov, I. A. Sadykov, Igor O. Shamshin
Publikováno v:
Shock Waves. 30:221-234
A water transportation engine of a new type—a pulsed detonation hydroramjet (PDH)—has been designed, manufactured, and tested. The PDH is a pulsed detonation tube (DT) inserted in an open-ended water guide. The thrust is developed by shock-induce
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::53c65cbffd4198e0c741c7b3f2e2ccf8
https://doi.org/10.1007/s00193-019-00906-2
https://doi.org/10.1007/s00193-019-00906-2
Publikováno v:
Aerospace Science and Technology. 89:275-287
The air-breathing pulsed detonation thrust module (TM) for an aircraft designed for a subsonic flight at a speed of up to 120 m/s when operating on a standard aviation kerosene was developed using the analytical estimates and parametric multivariant
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::596e9606375a2fbc8cc93b15ab238f21
https://doi.org/10.1016/j.ast.2019.04.005
https://doi.org/10.1016/j.ast.2019.04.005
Autor:
Igor O. Shamshin, Michail I. Alymov, V. A. Zelensky, V. S. Aksenov, E. V. Evstratov, S. M. Frolov, P. A. Gusev
Publikováno v:
Combustion Science and Technology. 192:144-165
The possibility of organizing a continuous-detonation combustion of a liquid fuel film in an annular combustor of a detonation liquid-propellant rocket engine has been demonstrated. The nea...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ae87d5f14286d0ed51a22c4439cb05c6
https://doi.org/10.1080/00102202.2018.1557643
https://doi.org/10.1080/00102202.2018.1557643