Standard
Tests of the hydrogen-fueled detonation ramjet model in a wind tunnel with thrust measurements. / Frolov, S. M.; Zvegintsev, V. I.; Ivanov, V. S. и др.
Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. ред. / Fomin. Том 1893 American Institute of Physics Inc., 2017. 020003 (AIP Conference Proceedings; Том 1893).
Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование
Harvard
Frolov, SM, Zvegintsev, VI, Ivanov, VS, Aksenov, VS, Shamshin, IO, Vnuchkov, DA, Nalivaichenko, DG, Berlin, AA
& Fomin, VM 2017,
Tests of the hydrogen-fueled detonation ramjet model in a wind tunnel with thrust measurements. в Fomin (ред.),
Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. Том. 1893, 020003, AIP Conference Proceedings, Том. 1893, American Institute of Physics Inc., 25th Conference on High-Energy Processes in Condensed Matter, HEPCM 2017, Novosibirsk, Российская Федерация,
05.06.2017.
https://doi.org/10.1063/1.5007441APA
Frolov, S. M., Zvegintsev, V. I., Ivanov, V. S., Aksenov, V. S., Shamshin, I. O., Vnuchkov, D. A., Nalivaichenko, D. G., Berlin, A. A.
, & Fomin, V. M. (2017).
Tests of the hydrogen-fueled detonation ramjet model in a wind tunnel with thrust measurements. в Fomin (Ред.),
Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS (Том 1893). [020003] (AIP Conference Proceedings; Том 1893). American Institute of Physics Inc..
https://doi.org/10.1063/1.5007441Vancouver
Frolov SM, Zvegintsev VI, Ivanov VS, Aksenov VS, Shamshin IO, Vnuchkov DA и др.
Tests of the hydrogen-fueled detonation ramjet model in a wind tunnel with thrust measurements. в Fomin, Редактор, Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. Том 1893. American Institute of Physics Inc. 2017. 020003. (AIP Conference Proceedings). doi: 10.1063/1.5007441
Author
BibTeX
@inproceedings{6b6914c2357e4c52b1303611037786fa,
title = "Tests of the hydrogen-fueled detonation ramjet model in a wind tunnel with thrust measurements",
abstract = "Experimental studies of an axisymmetric hydrogen-fueled detonation ramjet model 1.05-meter long and 0.31 m in diameter with an expanding annular combustor were performed in a pulse wind tunnel under conditions of approaching air stream Mach number ranging from 4 to 8 with the stagnation temperature of 293 K. In a supersonic air flow entering the combustor, continuous and longitudinally pulsating modes of hydrogen detonation with the corresponding characteristic frequencies of 1250 and 900 Hz were obtained. The maximum measured values of the fuel-based specific impulse and total thrust were 3600 s and 2200 N.",
keywords = "EXPERIMENTAL PROOF, ENERGY EFFICIENCY, COMBUSTOR, AIR, PROPULSION, ENGINE, CYCLE",
author = "Frolov, {S. M.} and Zvegintsev, {V. I.} and Ivanov, {V. S.} and Aksenov, {V. S.} and Shamshin, {I. O.} and Vnuchkov, {D. A.} and Nalivaichenko, {D. G.} and Berlin, {A. A.} and Fomin, {V. M.}",
year = "2017",
month = oct,
day = "26",
doi = "10.1063/1.5007441",
language = "English",
volume = "1893",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Fomin",
booktitle = "Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017",
note = "25th Conference on High-Energy Processes in Condensed Matter, HEPCM 2017 ; Conference date: 05-06-2017 Through 09-06-2017",
}
RIS
TY - GEN
T1 - Tests of the hydrogen-fueled detonation ramjet model in a wind tunnel with thrust measurements
AU - Frolov, S. M.
AU - Zvegintsev, V. I.
AU - Ivanov, V. S.
AU - Aksenov, V. S.
AU - Shamshin, I. O.
AU - Vnuchkov, D. A.
AU - Nalivaichenko, D. G.
AU - Berlin, A. A.
AU - Fomin, V. M.
PY - 2017/10/26
Y1 - 2017/10/26
N2 - Experimental studies of an axisymmetric hydrogen-fueled detonation ramjet model 1.05-meter long and 0.31 m in diameter with an expanding annular combustor were performed in a pulse wind tunnel under conditions of approaching air stream Mach number ranging from 4 to 8 with the stagnation temperature of 293 K. In a supersonic air flow entering the combustor, continuous and longitudinally pulsating modes of hydrogen detonation with the corresponding characteristic frequencies of 1250 and 900 Hz were obtained. The maximum measured values of the fuel-based specific impulse and total thrust were 3600 s and 2200 N.
AB - Experimental studies of an axisymmetric hydrogen-fueled detonation ramjet model 1.05-meter long and 0.31 m in diameter with an expanding annular combustor were performed in a pulse wind tunnel under conditions of approaching air stream Mach number ranging from 4 to 8 with the stagnation temperature of 293 K. In a supersonic air flow entering the combustor, continuous and longitudinally pulsating modes of hydrogen detonation with the corresponding characteristic frequencies of 1250 and 900 Hz were obtained. The maximum measured values of the fuel-based specific impulse and total thrust were 3600 s and 2200 N.
KW - EXPERIMENTAL PROOF
KW - ENERGY EFFICIENCY
KW - COMBUSTOR
KW - AIR
KW - PROPULSION
KW - ENGINE
KW - CYCLE
UR - http://www.scopus.com/inward/record.url?scp=85034273875&partnerID=8YFLogxK
U2 - 10.1063/1.5007441
DO - 10.1063/1.5007441
M3 - Conference contribution
AN - SCOPUS:85034273875
VL - 1893
T3 - AIP Conference Proceedings
BT - Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017
A2 - Fomin, null
PB - American Institute of Physics Inc.
T2 - 25th Conference on High-Energy Processes in Condensed Matter, HEPCM 2017
Y2 - 5 June 2017 through 9 June 2017
ER -
