On the public citation graph

Effects of ignition condition on the initiation characteristics of rotating detonation wave in plane-radial structure

https://doi.org/10.1016/j.actaastro.2020.05.052

0 signed · 80 inferred · view as graph

Inferred edges come from two machine sources: sweeps of open repository metadata (mostly SSRN and Zenodo), and a bulk OpenAlex citation snapshot. Every row below is labelled with the one it came from. Neither is a complete citation index — absence here is not evidence of absence.

Is this your work? Sign in with ORCID and put your name on the claims that are yours.

Claim with ORCID

Reference health. See whether every reference in this work resolves to a known work and none has been retracted — and get a dated CiteStamped badge you can embed.

See reference health

What this work says

Outgoing claims: the papers this work cites, builds on, or argues with.

inferredcites →https://doi.org/10.1007/s00193-011-0298-yopenalex-snapshot

Experimental research on the rotating detonation in gaseous fuels–oxygen mixtures

inferredcites →https://doi.org/10.1007/s10573-006-0076-9openalex-snapshot

Continuous spin detonation of fuel-air mixtures

inferredcites →https://doi.org/10.1016/j.actaastro.2017.07.024openalex-snapshot

Investigation on the propagation process of rotating detonation wave

inferredcites →https://doi.org/10.1016/j.actaastro.2019.01.009openalex-snapshot

Experimental investigation on propagation characteristics of rotating detonation wave with a hydrogen-ethylene-acetylene fuel

inferredcites →https://doi.org/10.1016/j.actaastro.2019.02.016openalex-snapshot

Three-dimensional modeling of rotating detonation in a ramjet engine

inferredcites →https://doi.org/10.1016/j.actaastro.2019.03.067openalex-snapshot

Effects of air injection throat width on a non-premixed rotating detonation engine

inferredcites →https://doi.org/10.1016/j.actaastro.2019.05.035openalex-snapshot

Rotating detonation engines with two fuel orifice schemes

inferredcites →https://doi.org/10.1016/j.actaastro.2019.08.007openalex-snapshot

Effect of blockage ratio on the existence of multiple waves in rotating detonation engine

inferredcites →https://doi.org/10.1016/j.actaastro.2019.09.038openalex-snapshot

Effects of cavity depth on the ethylene-air Continuous Rotating Detonation

inferredcites →https://doi.org/10.1016/j.actaastro.2019.12.022openalex-snapshot

Effects of flow-field structures on the stability of rotating detonation ramjet engine

inferredcites →https://doi.org/10.1016/j.applthermaleng.2017.10.146openalex-snapshot

The feasibility of mode control in rotating detonation engine

inferredcites →https://doi.org/10.1016/j.ast.2015.04.006openalex-snapshot

Experimental research on rotating detonation in liquid fuel–gaseous air mixtures

inferredcites →https://doi.org/10.1016/j.ast.2018.08.003openalex-snapshot

Rotating detonation in a ramjet engine three-dimensional modeling

inferredcites →https://doi.org/10.1016/j.ast.2018.12.014openalex-snapshot

A hollow combustor that intensifies rotating detonation

inferredcites →https://doi.org/10.1016/j.ast.2019.01.040openalex-snapshot

Experimental investigation on delay time phenomenon in rotating detonation engine

inferredcites →https://doi.org/10.1016/j.ast.2019.07.011openalex-snapshot

Performance analysis of dual-duct rotating detonation aero-turbine engine

inferredcites →https://doi.org/10.1016/j.combustflame.2014.09.023openalex-snapshot

Three-dimensional numerical investigations of the rotating detonation engine with a hollow combustor

inferredcites →https://doi.org/10.1016/j.expthermflusci.2014.11.017openalex-snapshot

An experimental study on CH4/O2 continuously rotating detonation wave in a hollow combustion chamber

inferredcites →https://doi.org/10.1016/j.expthermflusci.2017.11.002openalex-snapshot

Study of the ignition process in a laboratory scale rotating detonation engine

inferredcites →https://doi.org/10.1016/j.expthermflusci.2017.12.004openalex-snapshot

Rotating detonation wave mechanics through ethylene-air mixtures in hollow combustors, and implications to high frequency combustion instabilities

inferredcites →https://doi.org/10.1016/j.expthermflusci.2019.01.032openalex-snapshot

Experimental investigation on the propagation mode of rotating detonation wave in plane-radial combustor

inferredcites →https://doi.org/10.1016/j.ijhydene.2015.03.128openalex-snapshot

Experimental proof of Zel'dovich cycle efficiency gain over cycle with constant pressure combustion for hydrogen–oxygen fuel mixture

inferredcites →https://doi.org/10.1016/j.ijhydene.2017.09.015openalex-snapshot

Reinitiation phenomenon in hydrogen-air rotating detonation engine

inferredcites →https://doi.org/10.1016/j.ijhydene.2018.08.064openalex-snapshot

Experimental research on ignition, quenching, reinitiation and the stabilization process in rotating detonation engine

inferredcites →https://doi.org/10.1016/j.ijhydene.2019.11.014openalex-snapshot

Numerical investigation on H2/Air non-premixed rotating detonation engine under different equivalence ratios

inferredcites →https://doi.org/10.1016/j.proci.2016.07.097openalex-snapshot

Experimental study of the structure of forward-tilting rotating detonation waves and highly maintained combustion chamber pressure in a disk-shaped combustor

inferredcites →https://doi.org/10.1016/j.proci.2018.05.072openalex-snapshot

Effect of increasing channel width on the structure of rotating detonation wave

inferredcites →https://doi.org/10.1016/j.proci.2018.07.070openalex-snapshot

Critical condition of inner cylinder radius for sustaining rotating detonation waves in rotating detonation engine thruster

inferredcites →https://doi.org/10.1016/j.proci.2018.09.024openalex-snapshot

Three-dimensional numerical thrust performance analysis of hydrogen fuel mixture rotating detonation engine with aerospike nozzle

inferredcites →https://doi.org/10.1016/j.proci.2018.09.036openalex-snapshot

Investigation of the structure of detonation waves in a non-premixed hydrogen–air rotating detonation engine using mid-infrared imaging

inferredcites →https://doi.org/10.1051/eucass/201102555openalex-snapshot

Experimental and numerical study of the rotating detonation engine in hydrogen-air mixtures

inferredcites →https://doi.org/10.1088/1742-6596/1128/1/012075openalex-snapshot

Detonation of a hydrogen-oxygen gas mixture in a plane-radial combustor with exhaustion toward the periphery in the regime of oxygen ejection

inferredcites →https://doi.org/10.1134/s0010508211040113openalex-snapshot

Detonation of a coal-air mixture with addition of hydrogen in plane-radial vortex chambers

inferredcites →https://doi.org/10.1134/s0010508212020098openalex-snapshot

Detonation combustion of coal

inferredcites →https://doi.org/10.1134/s0010508213060105openalex-snapshot

Continuous spin detonation of a coal-air mixture in a flow-type plane-radial combustor

inferredcites →https://doi.org/10.1134/s1028335810030092openalex-snapshot

Continuous and pulsed detonation of a coal-air mixture

inferredcites →https://doi.org/10.2514/1.17656openalex-snapshot

Continuous Spin Detonations

inferredcites →https://doi.org/10.2514/1.b36213openalex-snapshot

Experimental Performance Scaling of Rotating Detonation Engines Operated on Gaseous Fuels

inferredcites →https://doi.org/10.2514/1.b36432openalex-snapshot

Low-Order Parametric Analysis of a Rotating Detonation Engine in Rocket Mode

inferredcites →https://doi.org/10.2514/6.2015-0878openalex-snapshot

Visualization of Rotating Detonation Waves in a Plane Combustor with a Cylindrical Wall Injector

inferredcites →https://doi.org/10.2514/6.2016-0126openalex-snapshot

Starting Transients and Detonation Onset Behavior in a Rotating Detonation Combustor

inferredcites →https://doi.org/10.2514/6.2016-5103openalex-snapshot

Experimental Study of Research of Centrifugal-Compressor-Radial-Turbine Type Rotating Detonation Engine

inferredcites →https://doi.org/10.2514/6.2017-1286openalex-snapshot

Experimental Study of the Disk-Shaped Rotating Detonation Turbine Engine

inferredcites →https://doi.org/10.2514/masm15openalex-snapshot

53rd AIAA Aerospace Sciences Meeting

inferredcites →https://doi.org/10.2514/masm16openalex-snapshot

54th AIAA Aerospace Sciences Meeting

inferredcites →https://doi.org/10.2514/mjpc16openalex-snapshot

52nd AIAA/SAE/ASEE Joint Propulsion Conference

What points at this work

Incoming claims: where this work appears in other papers’ reference lists and arguments.

inferred← citeshttps://doi.org/10.2139/ssrn.4499170openalex-extracted

Numerical Study on Rotating Detonation Combustion with the Discrete Distribution of Pre-Vaporized N-Heptane Sprays

inferred← citeshttps://doi.org/10.1002/ese3.1247openalex-snapshot

Experimental study on the effect of injection pressure ratio on the propagation characteristics of hydrogen rotating detonation waves

inferred← citeshttps://doi.org/10.1016/j.actaastro.2021.07.019openalex-snapshot

A rotating detonation engine using methane-ethylene mixture and air

inferred← citeshttps://doi.org/10.1016/j.actaastro.2021.11.035openalex-snapshot

Safety of a rotating detonation engine fed by acetylene – oxygen mixture launching stage

inferred← citeshttps://doi.org/10.1016/j.actaastro.2021.12.026openalex-snapshot

Numerical research on two-phase kerosene/air rotating detonation engines

inferred← citeshttps://doi.org/10.1016/j.actaastro.2022.01.002openalex-snapshot

Effects of supersonic nozzle guide vanes on the performance and flow structures of a rotating detonation combustor

inferred← citeshttps://doi.org/10.1016/j.actaastro.2022.02.015openalex-snapshot

Numerical simulations of vapor kerosene/air rotating detonation engines with different slot inlet configurations

inferred← citeshttps://doi.org/10.1016/j.actaastro.2022.03.003openalex-snapshot

Effects of the oxygen mass fraction on the wave propagation modes in a kerosene-fueled rotating detonation combustor

inferred← citeshttps://doi.org/10.1016/j.actaastro.2022.11.051openalex-snapshot

Effects of a straight guide vane on the operating characteristics of rotating detonation combustor

inferred← citeshttps://doi.org/10.1016/j.actaastro.2023.03.013openalex-snapshot

Impact of mixture mass flux on hydrodynamic blockage ratio and Mach number of rotating detonation combustor

inferred← citeshttps://doi.org/10.1016/j.actaastro.2023.07.011openalex-snapshot

Experimental research on the detonation behavior in annular combustors utilizing liquid hypergolic propellants

inferred← citeshttps://doi.org/10.1016/j.actaastro.2023.12.047openalex-snapshot

Experimental investigation on a rotating detonation combustor with the pulse operating frequency of 10 Hz

inferred← citeshttps://doi.org/10.1016/j.actaastro.2025.06.035openalex-snapshot

Design and ignition characteristics of kerosene/oxygen pre-detonator and kerosene/air hot-jet schemes under rotating detonation engine

inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2025.128779openalex-snapshot

Initiation characteristics of a rotating detonation combustor considering turbine effects using high-order dynamic mode decomposition

inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2026.132248openalex-snapshot

Effects of ignition conditions on detonation wave evolution in a rotating detonation engine

inferred← citeshttps://doi.org/10.1016/j.ast.2021.107300openalex-snapshot

Design and optimization of aerospike nozzle for rotating detonation engine

inferred← citeshttps://doi.org/10.1016/j.ast.2022.107661openalex-snapshot

Spinning pulsed detonation in rotating detonation engine

inferred← citeshttps://doi.org/10.1016/j.ast.2023.108676openalex-snapshot

Propagation behaviors of kerosene-fueled rotating detonation wave with varied atomizer locations

inferred← citeshttps://doi.org/10.1016/j.ast.2025.109955openalex-snapshot

The ignition and self-sustaining combustion of the rotating detonation fueled by solid propellant

inferred← citeshttps://doi.org/10.1016/j.combustflame.2024.113437openalex-snapshot

Initiation process of non-premixed continuous rotating detonation wave through Schlieren visualization

inferred← citeshttps://doi.org/10.1016/j.combustflame.2026.115323openalex-snapshot

Initiation pathways in non-premixed methane/oxygen rotating detonation combustors with hollow and annular chambers

inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2024.111389openalex-snapshot

Effects of employing supplemental oxygen in the ignition process on the initiation of rotating detonations

inferred← citeshttps://doi.org/10.1016/j.fuel.2022.125956openalex-snapshot

Characteristics of rotating detonation waves in a hollow chamber with different fuel injection positions

inferred← citeshttps://doi.org/10.1016/j.fuel.2023.129408openalex-snapshot

Experimental investigation on pulse operation characteristics of rotating detonation rocket engine

inferred← citeshttps://doi.org/10.1016/j.fuel.2023.129424openalex-snapshot

Study of the characteristics and combustion efficiency of liquid kerosene/oxygen-enriched air rotating detonation wave with different modes

inferred← citeshttps://doi.org/10.1016/j.fuel.2023.129650openalex-snapshot

Numerical study on rotating detonation combustion with the discrete distribution of partially pre-vaporized n-heptane sprays

inferred← citeshttps://doi.org/10.1016/j.jppr.2022.02.002openalex-snapshot

Investigation on C2H4-Air combustion mode in a non-premixed rotating detonation combustor

inferred← citeshttps://doi.org/10.1016/j.proci.2026.106577openalex-snapshot

Optical and pressure measurements of a premixed rotating detonation combustor with a porous injector

inferred← citeshttps://doi.org/10.1063/5.0077098openalex-snapshot

Analysis of flow-field characteristics and pressure gain in air-breathing rotating detonation combustor

inferred← citeshttps://doi.org/10.1063/5.0144322openalex-snapshot

Experimental study on the auto-initiation of rotating detonation with high-temperature hydrogen-rich gas

inferred← citeshttps://doi.org/10.1080/00102202.2024.2392644openalex-snapshot

Study on the Effects of Inflow Parameters on the Auto-Initiation of Hydrogen-Rich Gas Rotating Detonation

inferred← citeshttps://doi.org/10.1134/s0010508223050131openalex-snapshot

Droplet Size Impact on n-Heptane Detonation

inferred← citeshttps://doi.org/10.2514/1.b40326openalex-snapshot

Experimental Investigation on Dilution of Disk-Shaped Pressure Gain Combustor Exhaust

inferred← citeshttps://doi.org/10.2514/1.j061549openalex-snapshot

Effects of Divergence Inlet on Kerosene/Air Rotating Detonation Engines

Editorial review for independent work. ICSAC — the Institute for Complexity Science and Advanced Computing — runs a structured editorial panel for researchers publishing outside journals, and publishes on CiteStamp rails. Submission is free and goes through ORCID: icsacinstitute.org/submit.