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Inverse heat transfer method applied to capacitively cooled rocket thrust chambers

International journal of heat and mass transfer, 2019-03, Vol.131, p.150-166

2019

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Heat flux evaluation in a multi-element CH4/O2 rocket combustor using an inverse heat transfer method

International journal of heat and mass transfer, 2019-10, Vol.142, p.118425, Article 118425

2019

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Wall heat transfer prediction in CH4/O2 and H2/O2 rocket thrust chambers using a non-adiabatic flamelet model

Acta astronautica, 2020-09, Vol.174, p.254-269

2020

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An integrative SPH method for heat transfer problems involving fluid-structure interaction

Acta mechanica Sinica, 2023-02, Vol.39 (2), Article 722248

English ed., 2023

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Effects of near wall flow and non-equilibrium reaction coupling on heat flux prediction inside a 7-elements GOX/GCH4 combustion chamber

Applied thermal engineering, 2022-03, Vol.204, p.118021, Article 118021

2022

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Thermal behavior in the cracking reaction zone of scramjet cooling channels at different channel aspect ratios

Acta astronautica, 2016-10, Vol.127, p.41-56

2016

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Numerical study of film cooling in single-element injector gaseous CH4/O2 rocket engine with coupled wall function

AIP advances, 2024-03, Vol.14 (3), p.035330-035330-11

2024

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Experimental lifetime study of regeneratively cooled rocket chamber walls

International journal of fatigue, 2020-09, Vol.138, p.105649-12, Article 105649

2020

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Supervised learning mixing characteristics of film cooling in a rocket combustor using convolutional neural networks

Acta astronautica, 2020-10, Vol.175, p.11-18

2020

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Generative adversarial networks with physical evaluators for spray simulation of pintle injector

AIP advances, 2021-07, Vol.11 (7), p.075007-075007-11

2021

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Interactions Between Flame Topology and Turbulent Transport in High-Pressure Premixed Combustion

Flow, turbulence and combustion, 2022-09, Vol.109 (3), p.813-838

2022

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Modeling Investigation of Liquid Oxygen Flashing Spray with CFD

Journal of physics. Conference series, 2022-05, Vol.2235 (1), p.12061

2022

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Jet A and Propane gas combustion in a turboshaft engine: performance and emissions reductions

SN applied sciences, 2021-04, Vol.3 (4), p.471, Article 471

2021

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Numerical investigation of rocket engine cooling channel heat transfer for different LNG under trans-critical conditions

International Journal of Thermofluids, 2023-11, Vol.20, p.100461, Article 100461

2023

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Combustion of Kerosene Jet A Fuel and Superheated Steam Injection in an Aviation Turboshaft Engine: Improving Power Output and Reducing Emissions

Journal of the Institution of Engineers (India) Series C, 2021-04, Vol.102 (2), p.275-281

2021

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Influence of Mass Flow Rate on the Atomization Characteristics of Screw Conveyor Swirl Injectors

Aerospace, 2022-06, Vol.9 (6), p.293

2022

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An experimental and modelling study of heat loads on a subscale methane rocket motor

Acta astronautica, 2019-11, Vol.164, p.112-120

2019

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The Confirmation of Thermal Boundary Parameters in an Oxygen Kerosene Fuel-Rich Rocket Engine

Aerospace, 2022-07, Vol.9 (7), p.343

2022

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Combustion Regimes in Turbulent Non-Premixed Flames for Space Propulsion

Aerospace, 2023-08, Vol.10 (8), p.671

2023

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An Eddy Dissipation Concept Performance Study for Space Propulsion Applications

Aerospace, 2022-09, Vol.9 (9), p.476

2022

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Characterisation and Design of Direct Numerical Simulations of Turbulent Statistically Planar Flames

Aerospace, 2022-10, Vol.9 (10), p.530

2022

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Future Space-Transport-System Components under High Thermal and Mechanical Loads: Results from the DFG Collaborative Research Center TRR40

1st Edition 2021, 2020

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Impact of impurities on liquid methane properties under typical rocket operation conditions

International Journal of Thermofluids, 2023-05, Vol.18, p.100343, Article 100343

2023

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A comprehensive kinetic modeling study of hydrogen combustion with uncertainty quantification

Fuel (Guildford), 2022-07, Vol.319, p.123705, Article 123705

2022

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Multi-Phase Impact on the Heat Load Characteristics of a Multi-Element Methane-Oxygen Rocket Thrust Chamber

International journal of heat and mass transfer, 2021-06, Vol.172, p.121113, Article 121113

2021

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Inverse heat transfer method applied to capacitively cooled rocket thrust chambers

Heat flux evaluation in a multi-element CH4/O2 rocket combustor using an inverse heat transfer method

Wall heat transfer prediction in CH4/O2 and H2/O2 rocket thrust chambers using a non-adiabatic flamelet model

An integrative SPH method for heat transfer problems involving fluid-structure interaction

Effects of near wall flow and non-equilibrium reaction coupling on heat flux prediction inside a 7-elements GOX/GCH4 combustion chamber

Thermal behavior in the cracking reaction zone of scramjet cooling channels at different channel aspect ratios

Numerical study of film cooling in single-element injector gaseous CH4/O2 rocket engine with coupled wall function

Experimental lifetime study of regeneratively cooled rocket chamber walls

Supervised learning mixing characteristics of film cooling in a rocket combustor using convolutional neural networks

Generative adversarial networks with physical evaluators for spray simulation of pintle injector

Interactions Between Flame Topology and Turbulent Transport in High-Pressure Premixed Combustion

Modeling Investigation of Liquid Oxygen Flashing Spray with CFD

Jet A and Propane gas combustion in a turboshaft engine: performance and emissions reductions

Numerical investigation of rocket engine cooling channel heat transfer for different LNG under trans-critical conditions

Combustion of Kerosene Jet A Fuel and Superheated Steam Injection in an Aviation Turboshaft Engine: Improving Power Output and Reducing Emissions

Influence of Mass Flow Rate on the Atomization Characteristics of Screw Conveyor Swirl Injectors

An experimental and modelling study of heat loads on a subscale methane rocket motor

The Confirmation of Thermal Boundary Parameters in an Oxygen Kerosene Fuel-Rich Rocket Engine

Combustion Regimes in Turbulent Non-Premixed Flames for Space Propulsion

An Eddy Dissipation Concept Performance Study for Space Propulsion Applications

Characterisation and Design of Direct Numerical Simulations of Turbulent Statistically Planar Flames

Future Space-Transport-System Components under High Thermal and Mechanical Loads: Results from the DFG Collaborative Research Center TRR40

Impact of impurities on liquid methane properties under typical rocket operation conditions

A comprehensive kinetic modeling study of hydrogen combustion with uncertainty quantification

Multi-Phase Impact on the Heat Load Characteristics of a Multi-Element Methane-Oxygen Rocket Thrust Chamber

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