Effect of Hydrogen Peroxide Addition on the Modal and Thermochemical Response of a Hydrogen–Oxygen Rotating Detonation Engine

Abstract Rotating detonation engines (RDE) are compact pressure-gain combustors whose practical operation depends on maintaining coherent coupling among rotating-wave propagation, mixture replenishment, ignition, and heat release. This computational study examines whether a low-level hydrogen peroxide ( H 2 O 2 ) addition can act as a reactivity modifier in a nitrogen-diluted H 2 / O 2 RDE. Five 2D unwrapped-domain simulations are compared: a baseline case without H 2 O 2 and four additive cases from 1% to 4%, with the geometry, boundary conditions, initialization, mesh, and numerical settings kept fixed. The baseline case sustains a single rotating detonation wave and provides the reference state for the additive sweep. For 1%–3% H 2 O 2 , the combustor response changes only modestly: the dominant pressure frequency and frequency-inferred wave speed increase slightly; but pressure amplitude, cycle regularity, near Zel’dovich–von Neumann–Döring (ZND) pressure persistence, cumulative heat release, and supplied-mass-normalized heat release remain bounded and nonmonotonic. At 4% H 2 O 2 , the combustor transitions to a weaker dual-wave detonation mode. Although the dominant pressure frequency nearly doubles, the frequency-inferred wave speed decreases relative to its corresponding ideal Chapman–Jouguet velocity, and the pressure amplitude, near-ZND pressure persistence, pressure–heat-release timing consistency, and heat-release intensity all weaken. Region-level species diagnostics show that the 4% case has the largest mean OH and aggregate radical pool, but this reactive radical pool does not translate into stronger pressure or heat-release coupling. Within this controlled numerical configuration, the results show that H 2 O 2 -induced chemical sensitization alone does not guarantee improved RDE operation. The findings therefore suggest that additive levels should be assessed as coupled combustor states, using modal, pressure, heat-release, and species/radical diagnostics rather than chemical reactivity arguments alone.

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Publication Details

Journal
Journal of Energy Engineering
Published
2026-10-17
DOI
https://doi.org/10.1061/jleed9.eyeng-7210
Primary Topic
Combustion and Detonation Processes
Type
article
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article

Effect of Hydrogen Peroxide Addition on the Modal and Thermochemical Response of a Hydrogen–Oxygen Rotating Detonation Engine

Efstathios-Al. Tingas, Chris Guiver, Joshua Maider, Minh-Bau Luong
Journal of Energy Engineering
Combustion and Detonation Processes
article

Effect of Hydrogen Peroxide Addition on the Modal and Thermochemical Response of a Hydrogen–Oxygen Rotating Detonation Engine

Efstathios-Al. Tingas, Chris Guiver, Joshua Maider, Minh-Bau Luong
article en

Abstract

Abstract Rotating detonation engines (RDE) are compact pressure-gain combustors whose practical operation depends on maintaining coherent coupling among rotating-wave propagation, mixture replenishment, ignition, and heat release. This computational study examines whether a low-level hydrogen peroxide ( H 2 O 2 ) addition can act as a reactivity modifier in a nitrogen-diluted H 2 / O 2 RDE. Five 2D unwrapped-domain simulations are compared: a baseline case without H 2 O 2 and four additive cases from 1% to 4%, with the geometry, boundary conditions, initialization, mesh, and numerical settings kept fixed. The baseline case sustains a single rotating detonation wave and provides the reference state for the additive sweep. For 1%–3% H 2 O 2 , the combustor response changes only modestly: the dominant pressure frequency and frequency-inferred wave speed increase slightly; but pressure amplitude, cycle regularity, near Zel’dovich–von Neumann–Döring (ZND) pressure persistence, cumulative heat release, and supplied-mass-normalized heat release remain bounded and nonmonotonic. At 4% H 2 O 2 , the combustor transitions to a weaker dual-wave detonation mode. Although the dominant pressure frequency nearly doubles, the frequency-inferred wave speed decreases relative to its corresponding ideal Chapman–Jouguet velocity, and the pressure amplitude, near-ZND pressure persistence, pressure–heat-release timing consistency, and heat-release intensity all weaken. Region-level species diagnostics show that the 4% case has the largest mean OH and aggregate radical pool, but this reactive radical pool does not translate into stronger pressure or heat-release coupling. Within this controlled numerical configuration, the results show that H 2 O 2 -induced chemical sensitization alone does not guarantee improved RDE operation. The findings therefore suggest that additive levels should be assessed as coupled combustor states, using modal, pressure, heat-release, and species/radical diagnostics rather than chemical reactivity arguments alone.

Journal of Energy EngineeringVol. 153(1)
Edinburgh Napier University (GB), Trường Đại học Khoa học và Công nghệ Hà Nội (VN), Hanoi University of Science and Technology (VN)
Affordable and clean energy
Openalex Percentile: Top 18%
Combustion and Detonation Processes
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