Hydrogen fuel rocket engines simulation using LOGOS code

Смирнов, Н.Н.; Бетелин, В. Б.; Shagaliev, R.M.; Никитин, В. Ф.; Belyakov, I.M.; Deryuguin, Yu.N.; Aksenov, S.V.; Korchazhkin, D.A.

doi:10.1016/j.ijhydene.2014.04.150

Cited by 471 publications

(54 citation statements)

References 21 publications

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“…Brayton cycle is adopted in scramjet combustors, and its thermodynamic efficiency is much lower than that of detonation combustion [2] . The inherent theoretical advantage of detonation combustion over deflagrative combustion, has promoted the investigations on advanced propulsion of detonation engines [3][4][5] , and therefore the performance of scramjets might be enhanced greatly if detonation combustion is realized in supersonic combustible mixtures in scramjet 3 combustors.…”

Section: Introductionmentioning

confidence: 99%

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Adaptive mesh refinement based simulations of three-dimensional detonation combustion in supersonic combustible mixtures with a detailed reaction model

Cai

Liang

Deiterding

et al. 2016

International Journal of Hydrogen Energy

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Although the overdrive degree of the 3D detonation is smaller than that of the 2D case, more complex and irregular detonation fronts can be observed in the 3D case compared with the 2D detonation, which is likely because of the propagation of transverse waves and collisions of triple lines in multi-directions in 3D detonations. After the hot jet is shut down, the newly formed 2D Chapman-Jouguet (CJ) detonation has almost the same characteristic parameters with the corresponding 3D case, indicating that the 2D instabilities can be perfectly preserved in 3D simulations. However, the slapping wave reflections on the side walls in the 3D detonation result in the second oscillation along with the main one, which presents stronger instabilities compared with the 2D case. The inherent stronger 3D instabilities is also verified through the quantitative comparison between the 2D and 3D cases where the 3D result always shows stronger fluctuations than the 2D case.

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Section: Introductionmentioning

confidence: 99%

“…The probability of detonation initiation and propagation in 4 supersonic combustible mixtures was firstly explored through 2D simulations using a simplified reaction model [34] in [35]. Secondly, in order to show its valuable functions for detonation initiation and propagation a systematic research of a hot jet was conducted [36] .…”

Section: Introductionmentioning

confidence: 99%

Adaptive mesh refinement based simulations of three-dimensional detonation combustion in supersonic combustible mixtures with a detailed reaction model

Cai

Liang

Deiterding

et al. 2016

International Journal of Hydrogen Energy

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show abstract

“…The idealized thermodynamic efficiencies of constant pressure, constant volume, and detonation are 27%, 47%, and 49%, respectively [1] . Due to the inherent theoretical advantage of detonation over deflagration, investigations on detonation based engines have been promoted significantly [2][3][4] .…”

Section: Introductionmentioning

confidence: 99%

Adaptive simulations of cavity-based detonation in supersonic hydrogen–oxygen mixture

Cai

Liang

Deiterding

et al. 2016

International Journal of Hydrogen Energy

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Two-dimensional reactive Euler equations with a detailed reaction modelwhere the molar ratio of the combustible mixture H2/O2/Ar is 2:1:7 under the condition of pressure 6.67 kPa and temperature 298 K, are solved numerically with adaptive mesh refinement method to investigate detonation combustion using a hot jet initiation in cavity-based channels filled with the supersonic combustible mixture.Results show that from the comparison between the simulations in a cavity-based channel and a straight channel without any cavity embedded, it is indicated that the cavity can help realize detonation initiation in the combustible mixture with a hot jet.It is suggested that detonation initiation can be realized using a relatively weaker hot jet in cavity-based channels filled with the supersonic combustible mixture compared with that in straight channels without a cavity embedded. The cavity also plays a significant role in detonation propagation in the supersonic combustible mixture.After the hot jet is shut down, the acoustic wave generated by the subsonic combustion in the cavity can accelerate detonation propagation through a subsonic Corresponding author. Email addresses: cai-chonger@hotmail.com, jhleon@vip.sina.com, r.deiterding@soton.ac.uk, linzy96@nudt.edu.cn, channel and result in the formation of a slightly overdriven detonation eventually. For a given flow with a shadow cavity embedded, there should exist a minimum cavity width Lmin. When the width is below Lmin, only some pressure oscillations in the cavity can make some impacts on detonation initiation and propagation. Otherwise, cavity oscillations can be generated which can greatly accelerate detonation initiation and propagation in the supersonic combustible mixture. For the shadow cavity, purely increasing the cavity depth does not have any more influence on detonation combustion. However, if the cavity is a deep one, it can play an important role in accelerating detonation initiation and propagation in the supersonic combustible mixture due to resonant oscillations.

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“…Propellant based on hydrogen peroxide has a number of advantages such as high density, non-toxic, high specific impulse and others. In order to use the hydrogen peroxide as a propellant it must be of high quality and above 90% concentration to reduce the decomposition on the surfaces of contact [6][7][8]. High-concentrated hydrogen peroxide is very insensitive to detonation by shock or impact.…”

Section: Introductionmentioning

confidence: 99%

Safety issues of high-concentrated hydrogen peroxide production used as rocket propellant

Romantsova

Ulybin

2015

Acta Astronautica

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Hydrogen fuel rocket engines simulation using LOGOS code

Cited by 471 publications

References 21 publications

Adaptive mesh refinement based simulations of three-dimensional detonation combustion in supersonic combustible mixtures with a detailed reaction model

Adaptive mesh refinement based simulations of three-dimensional detonation combustion in supersonic combustible mixtures with a detailed reaction model

Adaptive simulations of cavity-based detonation in supersonic hydrogen–oxygen mixture

Safety issues of high-concentrated hydrogen peroxide production used as rocket propellant

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