Fuel vapor and liquid condition is the critical factor for the suction feed, which is the basic function of the fuel system for civil aircraft. The suction feed function for some aircraft is verified as an example in this paper with the strict flight test method. Based on the test data, the vapor and liquid ratio (V/L) is calculated and the corresponding effect is analyzed. The research can be used on guiding aircraft fuel system design and engine performance evaluation.
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卞刚、朱德轩、张斌、郭军亮.燃油气液比对飞机吸力供油的影响研究[J].民用飞机设计与研 究,2015(1):23-Bian Gang、Zhu Dexuan、Zhang Bin、Guo Junliang. Impact Research of Fuel V/L on Aircraft Suction Feed[J]. Civil Aircraft Design and Research,2015,(1):23-. ( in Chinese)