Data-driven chemical kinetic reaction mechanism for F-24 jet fuel ignition
A data-driven chemical kinetic mechanism for the military version of Jet A, F-24, is
developed for numerical simulations of the ignition process. The main purpose of this study …
developed for numerical simulations of the ignition process. The main purpose of this study …
Constant volume combustion chamber (CVCC) investigations of aerospace F-24 and Jet-A in low-temperature heat release and negative temperature coefficient …
V Soloiu, A Weaver, L Parker, A Brant, R Smith III… - Energy Conversion and …, 2022 - Elsevier
A study was conducted to determine the characteristics of Low Temperature Heat Release,
Derived Cetane Number, and the Vibrations, produced by the combustion of aerospace F24 …
Derived Cetane Number, and the Vibrations, produced by the combustion of aerospace F24 …
Computational fluid dynamics and Machine learning-based Piston-Bowl optimization for Energy-Assisted compression ignition of low cetane number sustainable …
Hybrid-electric powertrains have been gaining tremendous interest to propel unmanned
aerial vehicles (UAVs) for Advanced Air Mobility. Present UAV powertrains are designed …
aerial vehicles (UAVs) for Advanced Air Mobility. Present UAV powertrains are designed …
Modeling of the spray-induced wall stress acting on the ignition assistance device
This research introduces a novel wall-stress model called the Spray-Induced Wall Stress
(SIWS) model, which considers the effects of spray-wall impingement and the resulting …
(SIWS) model, which considers the effects of spray-wall impingement and the resulting …
Transient Thermomechanical Stress Analysis of Hot Surface Ignition Device Using Sequentially Coupled Computational Fluid Dynamics–Finite Element Analysis …
Energy addition using a hot surface ignition device is required for reliable ignition of aircraft
compression ignition engines running on fuel variations and at altitude conditions. Thus …
compression ignition engines running on fuel variations and at altitude conditions. Thus …
Thermomechanical characterization of hot surface ignition device using phenomenological heat flux model
Modern aircraft compression ignition engines that seek to achieve fuel-flexible operation
require ignition-assisting devices to perform reliably. Many military propulsion systems, and …
require ignition-assisting devices to perform reliably. Many military propulsion systems, and …
Numerical investigations of combustion dynamics and thermo-mechanical stress in the ignition assistance system for small aircraft engines
The utilization of ignition assistance devices offers an effective solution to overcome the
challenges associated with ignition control in the development of propulsion systems for …
challenges associated with ignition control in the development of propulsion systems for …
Computational investigation of a methanol compression ignition engine assisted by a glow plug
This work explores the feasibility of pure methanol combustion in a light-duty diesel engine
assisted by a glow plug (GP). The simulations represented a mild engine load with an …
assisted by a glow plug (GP). The simulations represented a mild engine load with an …
Thermo-mechanical response of a hot surface ignition device under aircraft compression ignition engine conditions
View Video Presentation: https://doi. org/10.2514/6.2021-3615. vid Aircraft compression
ignition (CI) engines, originally developed for ground applications, exhibit significant ignition …
ignition (CI) engines, originally developed for ground applications, exhibit significant ignition …
Effect of hot probe temperature on ignition of alcohol-to-jet (Atj) fuel spray under aircraft propulsion system conditions
View Video Presentation: https://doi. org/10.2514/6.2021-0985. vid The effect of ignition
assistant probe temperature on ignition delay was investigated to achieve reliable …
assistant probe temperature on ignition delay was investigated to achieve reliable …