Relevant bibliographies by topics / Continuous spin detonations

Academic literature on the topic 'Continuous spin detonations'

Author: Grafiati
Published: 10 December 2022
Last updated: 29 January 2023

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Journal articles on the topic "Continuous spin detonations"

1

Bykovskii, Fedor A., Sergey A. Zhdan, and Evgenii F. Vedernikov. "Continuous Spin Detonations." Journal of Propulsion and Power 22, no. 6 (November 2006): 1204–16. http://dx.doi.org/10.2514/1.17656.

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Popov, E. L., A. N. Samsonov, F. A. Bykovskii, and E. F. Vedernikov. "MHD effects in continuous spin detonation." Доклады Академии наук 484, no. 5 (May 16, 2019): 550–53. http://dx.doi.org/10.31857/s0869-56524845550-553.

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Conversion possibility of the chemical energy of combustion products of a hydrogen–oxygen mixture into electrical energy with the use of continuous spin detonation has been demonstrated for the first time in an MHD system. The specific conductivity of detonation products in the region of rotation of the detonation front was measured to be ~3 · 10–2 Ω–1 m–1. The structure of transverse detonation waves was examined, their velocity was measured (2220 ± 50 m/s), and the flow in their vicinity was studied.
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3

Popov, E. L., A. N. Samsonov, F. A. Bykovskii, and E. F. Vedernikov. "MHD Effects in Continuous Spin Detonation." Doklady Physics 64, no. 2 (February 2019): 77–79. http://dx.doi.org/10.1134/s102833581902006x.

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4

Bykovskii, F. A., S. A. Zhdan, and E. F. Vedernikov. "Continuous Spin Detonation in Annular Combustors." Combustion, Explosion, and Shock Waves 41, no. 4 (July 2005): 449–59. http://dx.doi.org/10.1007/s10573-005-0055-6.

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5

Bykovskii, F. A., S. A. Zhdan, and E. F. Vedernikov. "Continuous spin detonation of fuel-air mixtures." Combustion, Explosion, and Shock Waves 42, no. 4 (July 2006): 463–71. http://dx.doi.org/10.1007/s10573-006-0076-9.

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6

Bykovskii, F. A., S. A. Zhdan, and E. F. Vedernikov. "Continuous spin detonation of synthesis gas-air mixtures." Combustion, Explosion, and Shock Waves 49, no. 4 (July 2013): 435–41. http://dx.doi.org/10.1134/s0010508213040060.

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Bykovskii, F. A., S. A. Zhdan, E. F. Vedernikov, and A. N. Samsonov. "Scaling factor in continuous spin detonation of syngas–air mixtures." Combustion, Explosion, and Shock Waves 53, no. 2 (March 2017): 187–98. http://dx.doi.org/10.1134/s0010508217020095.

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8

Trotsyuk, A. V. "Numerical modelling of continuous spin detonation in rich methane-oxygen mixture." Journal of Physics: Conference Series 754 (October 2016): 052006. http://dx.doi.org/10.1088/1742-6596/754/5/052006.

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9

Bykovskii, F. A., S. A. Zhdan, and E. F. Vedernikov. "Continuous spin detonation of hydrogen-oxygen mixtures. 1. Annular cylindrical combustors." Combustion, Explosion, and Shock Waves 44, no. 2 (March 2008): 150–62. http://dx.doi.org/10.1007/s10573-008-0021-1.

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10

Heister, Stephen D., John Smallwood, Alexis Harroun, Kevin Dille, Ariana Martinez, and Nathan Ballintyn. "Rotating Detonation Combustion for Advanced Liquid Propellant Space Engines." Aerospace 9, no. 10 (October 7, 2022): 581. http://dx.doi.org/10.3390/aerospace9100581.

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Rotating (also termed continuous spin) detonation technology is gaining interest in the global research and development community due to the potential for increased performance. Potential performance benefits, thrust chamber design, and thrust chamber cooling loads are analyzed for propellant applications using liquid oxygen or high-concentration hydrogen peroxide oxidizers with kerosene, hydrogen, and methane fuels. Performance results based on a lumped parameter treatment show that theoretical specific impulse gains of 3–14% are achievable with the highest benefit coming from hydrogen-fueled systems. Assessment of thrust chamber designs for notional space missions shows that both thrust chamber length and diameter benefits are achievable given the tiny annular chamber volume associated with the rotating detonation combustion. While the passing detonation front drastically increases local heat fluxes, global energy balances can be achieved if operating pressures are limited to be comparable to existing or prior space engines.
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Conference papers on the topic "Continuous spin detonations"

1

BYKOVSKII, F. A., S. A. ZHDAN, and E. F. VEDERNIKOV. "SPECIFIC IMPULSES FOR CONTINUOUS DETONATION OF METHANE/HYDROGEN-AIR MIXTURES." In 8TH INTERNATIONAL SYMPOSIUM ON NONEQUILIBRIUM PROCESSES, PLASMA, COMBUSTION, AND ATMOSPHERIC PHENOMENA. TORUS PRESS, 2020. http://dx.doi.org/10.30826/nepcap2018-2-24.

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Regimes of continuous spin detonation (CSD) with transverse detonation waves (TDWs) are obtained in a flow-type annular cylindrical combustor DK-500 for fuel-air mixtures (FAMs) with two compositions of the binary fuel CH4 + 8H2 and CH4 +4H2. Regimes of continuous multifront detonation (CMD) with colliding TDWs are obtained for the FAM with the CH4 + 2H2 binary fuel. These regimes are characterized by significant irregularity of the TDW structure and by a comparatively low TDW velocity. Specific impulses in continuous detonation are determined and analyzed for different compositions of the methane/hydrogen binary fuel. The maximum measured values of the specific impulse at the combustor exit are approximately 3800 s in CSD of CH4 + 8H2 and CH4 + 4H2, 3200 s in CMD of CH4 + 2H2, and 1600 s in combustion of CH4 + H2.
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2

Zhdan, S. A., A. I. Rybnikov, and E. V. Simonov. "Calculation of continuous spin detonation in a hydrogen-air mixture in an annular combustor." In INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2018). Author(s), 2018. http://dx.doi.org/10.1063/1.5065101.

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