Experimental and Analytical Characterization of Alternative Aviation Fuel Sprays Under Realistic Operating Conditions

燃油喷射 喷嘴 喷气燃料 校准 燃烧 航空 燃烧室 环境科学 工作(物理) 喷气发动机 核工程 机械工程 汽车工程 航空航天工程 工程类 物理 有机化学 化学 量子力学
作者
Andrew Corber,N. K. Rizk,Wajid A. Chishty
出处
期刊:Journal of engineering for gas turbines and power [ASM International]
卷期号:141 (6) 被引量:15
标识
DOI:10.1115/1.4041649
摘要

The National Jet Fuel Combustion Program (NJFCP) is an initiative being led by the Office of Environment & Energy at the FAA, to streamline the ASTM jet fuels certification process for alternative aviation fuels. To accomplish this, the program has identified specific applied research tasks in several areas. The National Research Council of Canada (NRC) is contributing to the NJFCP in the areas of sprays and atomization and high altitude engine performance. This paper describes work pertaining to atomization tests using a reference injection system. The work involves characterization of the injection nozzle, comparison of sprays and atomization quality of various conventional and alternative fuels, and uses the experimental data to validate spray correlations. The paper also briefly explores the application viability of a new diagnostic system that has the potential to reduce test time in characterizing sprays. Measurements were made from ambient up to 10 bar pressures in NRC's High Pressure Spray Facility using optical diagnostics including laser diffraction, phase Doppler anemometry (PDA), LIF/Mie imaging and laser sheet imaging to assess differences in the atomization characteristics of the test fuels. A total of nine test fluids including six NJFCP fuels and three calibration fluids were used. The experimental data were then used to validate semi-empirical models, developed through years of experience by engine original equipment manufacturers, and modified under the NJFCP, for predicting droplet size and distribution. The work offers effective tools for developing advanced fuel injectors, and generating data that can be used to significantly enhance multidimensional combustor simulation capabilities.
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