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Experimental Investigation on the Combustion Characteristics of Kerosene with Different Phases in Aero-engine Combustion Chambers

https://doi.org/10.2139/ssrn.6188883
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Experimental investigation of the nonlinear response of turbulent premixed flames to imposed inlet velocity oscillations
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Development and application of a three-parameter RK–PR equation of state
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High temperature fuel impacts on combustion characteristics of a swirl-stabilized combustor
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Effect of fuel temperature on the structure of a high-pressure liquid-fueled swirl flame
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Experimental assessment of the impact of variation in jet fuel properties on spray flame liftoff height
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Combustor technology of high temperature rise for aero engine
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CH∗ chemiluminescence modeling for combustion diagnostics
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Characterization of Combustion Chemiluminescence: An Image Processing Approach
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Crossing the Widom-line – Supercritical pseudo-boiling
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Spatially resolved measurement of OH*, CH*, and C2* chemiluminescence in the reaction zone of laminar methane/air premixed flames
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Supercritical (and subcritical) fluid behavior and modeling: drops, streams, shear and mixing layers, jets and sprays
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Frequency domain and time domain analysis of thermoacoustic oscillations with wave-based acoustics
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Time Series and Spectral Analysis of Thermoacoustic Oscillations for Propane-Oxyfuel Combustion in a Swirl-Stabilized, Nonpremixed Combustor
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Density Measurements of Endothermic Hydrocarbon Fuel at Sub- and Supercritical Conditions
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Viscosity Measurements of Endothermic Hydrocarbon Fuel from (298 to 788) K under Supercritical Pressure Conditions
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On the transition between two-phase and single-phase interface dynamics in multicomponent fluids at supercritical pressures
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A Correlation of the Viscosity and Thermal Conductivity Data of Gaseous and Liquid Ethylene
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Flame Sheet Imaging Using CH Chemiluminescence
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The use of fast Fourier transform for the estimation of power spectra: A method based on time averaging over short, modified periodograms
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Fuel-Cooled Thermal Management for Advanced Aeroengines
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Review of the Development of Compact, High Performance Heat Exchangers for Gas Turbine Applications
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Test results of the Northrop Grumman Corporation Turbine Engine Bleed Air/Fuel Heat Exchanger after 165 hours of operation with JP-8+100 fuel
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Gas Turbine Fuel System and Combustion Study with High Temperature Fuel Injection
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