Gotowe bibliografie tematyczne / Kerosene-PLIF

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  1. Artykuły w czasopismach
  2. Rozprawy doktorskie
  3. Streszczenia konferencji

Gotowa bibliografia na temat „Kerosene-PLIF”

Autor: Grafiati
Data publikacji: 29 marca 2025
Data aktualizacji: 31 lipca 2025

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Artykuły w czasopismach na temat "Kerosene-PLIF"

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Milea, Andrei Silviu, Aurélien Perrier, Marcos Caceres, et al. "Investigation On A Novel Injector Concept For Spinning Combustion Technology In High-Pressure Conditions By Advanced Laser-Based Diagnostics." Proceedings of the International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics 21 (July 8, 2024): 1–13. http://dx.doi.org/10.55037/lxlaser.21st.93.

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Safran Helicopter Engines has recently patented the spinning combustion technology in which the burnt gases from one injector travel tangentially along the combustor annulus towards the neighboring injectors. Compared to conventional designs, the new kerosene injection systems are dedicated to improve air/fuel mixture ignition but also to further reduce NOx and soot particle emissions. Experimental studies are performed on these fuel injectors in a high-pressure/high-temperature combustion facility designed by the CORIA research laboratory. This test bench is able to reproduce the same operati
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Yang, Hui, Feng Li, Bai Gang Sun, et al. "Schlieren and PLIF Measurements of Liquid Fuel Injection in Mach 2 Supersonic Crossflow." Advanced Materials Research 571 (September 2012): 701–5. http://dx.doi.org/10.4028/www.scientific.net/amr.571.701.

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Structures of liquid-fuel injection in supersonic crossflow is studied experimentally. Schemes of flush-wall injector and aviation kerosene are selected. The conditions of the supersonic freestream are kept constant (total pressure is 0.5MPa, total temperature is 500K and Mach number is 2) and the diameter of the injector is fixed as 0.5mm, while seven scenarios of injection angle and three scenarios of injection driven pressure are discussed. Both methods of schlieren and planar laser induced fluorescence (PLIF) techniques are implemented to obtain the visual images of the liquid-fuel injecti
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Wu, Yi, Vincent Modica, Xilong Yu, Fei Li, and Frédéric Grisch. "Effects of optical diagnostic techniques on the accuracy of laminar flame speeds measured from Bunsen flames: OH* chemiluminescence, OH-PLIF and acetone/kerosene-PLIF." Measurement Science and Technology 29, no. 1 (2017): 015204. http://dx.doi.org/10.1088/1361-6501/aa92d7.

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Xin, Shirong, Wenyu Wang, Yong He, Yanqun Zhu, and Zhihua Wang. "Effect of low fuel temperature on combustion deterioration of kerosene swirling spray flames using OH-PLIF." Fuel 358 (February 2024): 130098. http://dx.doi.org/10.1016/j.fuel.2023.130098.

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Xin, Shirong, Yong He, Tao Liu, Yingchun Wu, Xuecheng Wu, and Zhihua Wang. "Temperature and flame structure imaging in kerosene swirl-stabilized spray flames at low air flow using TLAF and OH-PLIF." Journal of the Energy Institute 109 (August 2023): 101294. http://dx.doi.org/10.1016/j.joei.2023.101294.

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Wu, Guohua, Xin Yu, Jiangbo Peng, et al. "Experimental investigation on the mixing and combustion characteristics with dual combined flame stabilizers in scramjet using simultaneous OH/kerosene-PLIF and Mie scattering measurements." Applied Thermal Engineering 277 (October 2025): 127004. https://doi.org/10.1016/j.applthermaleng.2025.127004.

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Malbois, P., E. Salaün, B. Rossow, et al. "Quantitative measurements of fuel distribution and flame structure in a lean-premixed aero-engine injection system by kerosene/OH-PLIF measurements under high-pressure conditions." Proceedings of the Combustion Institute 37, no. 4 (2019): 5215–22. http://dx.doi.org/10.1016/j.proci.2018.05.171.

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Tao, Chao, Chi Zhang, Qiang An, and Xin Xue. "Temperature Field Measurements in Swirl Spray Flames Using Two-Line Planar Laser Induced Fluorescence Thermometry." Journal of Engineering for Gas Turbines and Power, September 2, 2024, 1–17. http://dx.doi.org/10.1115/1.4066409.

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Abstract This paper investigates the temperature fields in a centrally staged swirl spray combustor using two-line OH planar laser induced fluorescence (PLIF) thermometry at elevated inlet pressures and temperatures up to 0.62 MPa and 650 K. The pilot and main stages of the combustor were supplied with RP-3 kerosene. OH radicals were excited using the Q1(5) and Q1(14) transitions within the A2Σ←X2Π (1,0) band. Two laser excitation systems were operated simultaneously, where the two beams were spatially combined and separated by a small interval in time. The PLIF signals excited at the two wave
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Shi, Si, Kevin J. Hughes, and Mohamed Pourkashanian. "A quantitative study of OH and NO concentration of a premixed laminar kerosene flame using a flat-flame burner at atmospheric pressure." Frontiers in Fuels 2 (November 18, 2024). http://dx.doi.org/10.3389/ffuel.2024.1401691.

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In the context of global warming and the increasing demands for the application of sustainable fuels, measurements of a variety of experimental targets under a wide range of conditions are crucial to improving the fundamental understanding of real jet fuels and developing quality kinetic mechanisms for large hydrocarbons. Planar laser-induced fluorescence (PLIF) is an effective approach to investigate concentrations of important species of a given flame while quantifying the fluorescence image remains a great challenge with significant uncertainties. This investigation aims to improve the fund
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Wu, Guohua, Xin Yu, Jiangbo Peng, et al. "Experimental investigation of lean blow-out on bluff-body stabilized flames using simultaneous OH/kerosene-PLIF measurements in partially vapourised kerosene." Experimental Thermal and Fluid Science, March 2025, 111458. https://doi.org/10.1016/j.expthermflusci.2025.111458.

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Rozprawy doktorskie na temat "Kerosene-PLIF"

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Milea, Andrei-Silviu. "Experimental investigation of innovative Low NOx / low soot injection systems for spinning combustiοn technology using advanced laser diagnostics". Electronic Thesis or Diss., Normandie, 2024. http://www.theses.fr/2024NORMIR43.

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Les effets anthropogéniques sur l’environnement posent un défi majeur pour l’industrie aéronautique. Des réglementations de plus en plus strictes et la nécessité de rendre le transport aérien durable orientent les recherches actuelles vers des systèmes propulsifs innovants. Dans ce contexte, Safran Helicopter Engines développe sa technologie brevetée de combustion giratoire (SCT), visant à améliorer les performances des moteurs d’hélicoptères. Déjà implémentée sur le moteur Arrano, cette technologie est davantage optimisée pour réduire significativement les émissions de NOx et de suies. Dans l
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Streszczenia konferencji na temat "Kerosene-PLIF"

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Milea, Andrei-Silviu, Aurélien Perrier, Marcos Caceres, et al. "Experimental Study of a Low NOx and Soot Injection System for Spinning Combustion Technology: Characterization of Soot and NO Formation Under Realistic Operating Conditions by Laser Diagnostics." In ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/gt2023-102769.

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Abstract In the context of air pollution, Safran Helicopter Engines patented an innovative design for helicopter combustors based on Spinning Combustion Technology. The development focuses on novel concepts of kerosene fuel injectors aiming to further reduce NOx and soot particle emissions. Experimental studies are performed on the fuel injectors in a high-pressure/high-temperature combustion facility designed by the CORIA laboratory. This test bench is able to reproduce the same conditions encountered in a helicopter combustor over the entire range of nominal operating conditions and has larg
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Salaün, E., F. Frindt, G. Cabot, et al. "Experimental Investigation on NO Pollutant Formation in High-Pressure Swirl-Stabilized Kerosene/Air Flames Using NO-, OH- and Kerosene-PLIF and PIV Laser Diagnostics." In ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/gt2020-14985.

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Abstract A Lean Premixed injection system (LP) was experimentally investigated at elevated pressure and air inlet temperature, corresponding to engine conditions, i.e. with high swirl number and elevated fresh gases velocities. OH-PLIF, NO-PLIF and kerosene-PLIF laser diagnostics were used to study the flame structure and the NO formation within the primary zone. These experimental studies were complemented with PIV measurements. The acquired data allows the evaluation of the coupling of aerodynamics with the flame structure. Starting from there, the combustion process governing the formation
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Li, Xi P., Weidong Liu, Leichao Yang, Jiajian Zhu, and Yu Pan. "Experimental investigation on fuel distribution using kerosene-PLIF in a scramjet combustor with dual cavity." In 21st AIAA International Space Planes and Hypersonics Technologies Conference. American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-2221.

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Tao, Chao, Chi Zhang, Qiang An, and Xin Xue. "Temperature Field Measurements in Swirl Spray Flames Using Two-Line Planar Laser Induced Fluorescence Thermometry." In ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2024. http://dx.doi.org/10.1115/gt2024-123973.

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Abstract This paper investigates the temperature fields in a centrally staged swirl spray combustor using two-line OH planar laser induced fluorescence (PLIF) thermometry at elevated inlet pressures and temperatures up to 0.62 MPa and 650 K. The pilot and main stages of the combustor were supplied with RP-3 kerosene. OH radicals were excited using the Q1(5) and Q1(14) transitions within the A2Σ←X2Π (1, 0) band. Two laser excitation systems were operated simultaneously, where the two beams were spatially combined and separated by a small interval in time. The PLIF signals excited at the two wav
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Jain, Ayush, Yejun Wang, Christian Schweizer, and Waruna D. Kulatilaka. "Investigation of Flow-Flame Interactions in Kerosene Piloted Liquid-Spray Flames Using Simultaneous OH and PAH PLIF." In AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-0525.

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Wang, Yejun, Tyler Paschal, and Waruna D. Kulatilaka. "Combustion Characterization of a Fuel-Flexible Piloted Liquid-Spray Flame Apparatus Using Advanced Laser Diagnostics." In ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/gt2019-91971.

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Abstract Primary energy sources for aviation gas turbines as well as direct-injection gasoline and diesel engines come in the form of liquid hydrocarbon fuels. These liquid fuels are atomized and mixed with air, prior to highly turbulent combustion and heat release processes inside engine hardware. Designing more efficient and cleaner gas turbine engines is hence dependent on the in-depth understanding of spray formation, mixing, heat release, combustion dynamics, and pollutant formation pathways in liquid-fuel spray flames. As compared to gaseous fuels, the additional steps of atomization, di
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Malbois, P., E. Salaun, F. Frindt, et al. "Experimental Investigation With Optical Diagnostics of a Lean-Premixed Aero-Engine Injection System Under Relevant Operating Conditions." In ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gt2017-64484.

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A Lean-Premixed (LP) aero-engine injection system was experimentally studied using optically-based measurements. Experiments were conducted under relevant operating conditions up to 1.38 MPa and using commercial kerosene as fuel. First of all, the structure of the reaction zone and the flame length into the combustion chamber have been studied with CH* chemiluminescence. It is observed from the data measurements that combustion can produce two types of flames, a V-shaped flame in which combustion is stabilized a few mm downstream from the injector and a tulip flame in which combustion is devel
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Renaud, Antoine, Shigeru Tachibana, Shuta Arase, and Takeshi Yokomori. "Experimental Study of Thermo-Acoustic Instability Triggering in a Staged Liquid Fuel Combustor Using High-Speed OH-PLIF." In ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gt2017-64102.

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A staged injector developed by JAXA and fueled with kerosene is studied in a high-pressure combustion experiment. With a stable pilot fuel flow rate, the fuel flow rate in the main stage is progressively increased. A high-speed OH-PLIF system is used to record the flame motion at 10,000 fps. In the beginning of the recording, POD modes shows that the flame behavior is dominated by relatively low-frequency rotation due to the swirling motion of the flow. These rotational motions then coexist with a thermo-acoustic instability around 475 Hz which increases the amplitude of the pressure fluctuati
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Yulan, Wang, Mu Yong, Fan Xiongjie, Zhao Qianpeng, and Xu Gang. "Injection of Kerosene Into a High-Temperature and High-Speed Air Crossflow." In ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/gt2020-15187.

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Abstract The jet of kerosene into high-temperature and high-speed air crossflow was studied experimentally, to study the characteristics of penetration and evaporation in afterburner. A fuel injection bar with a 0.6 mm diameter plain orifice was used in the experiment. The angle between jet and air flow was 90°. The tests were conducted at atmospheric pressure. The air temperature was between 400 °C to 800 °C, and the air velocity increased from 100 m/s to 250 m/s, which was close to the working condition of the afterburner. The jet flow rate also increased from 5 kg/h to 40 kg/h. Fuel-PLIF wa
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Wang, Zhichao, Xin Hui, Jianchen Wang, Yuzhen Lin, and Chi Zhang. "Effects of Axial Velocity of Main Stage on the Performances of a Centrally Staged LPP Combustor." In ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/gt2019-90933.

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Abstract Characteristics of the main stage exert important effects on the performances in a centrally staged LPP combustor. The experiments on flow fields, spray, and combustion were carried out on the combustors with different axial velocity at the main stage exit (Vm). The NOx emissions, combustion efficiency and lean blowout are all tested in a rectangular model combustor under elevated temperature and pressure conditions, while flow field and spray characteristics are measured in an optical combustor by Kerosene-PLIF and PIV under non-reacting elevated temperature and pressure conditions.
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