基于流体力学的吸力供油试飞方法分析  

Analysis of suction feed flight test methods based on fluid dynamics

作　　者：刘志远 夏树丹 任伟[1] LIU Zhiyuan;XIA Shudan;REN Wei

机构地区：[1]中国飞行试验研究院,陕西西安710089

出　　处：《现代机械》2017年第6期22-25,共4页Modern Machinery

摘　　要：飞机燃油系统试飞涉及众多学科,但没有专业书籍阐述其原理。从流体力学理论出发,结合GJB3212《飞机燃油系统飞行试验要求》,对飞机燃油系统吸力供油的试飞方法给出理论解释,以便其它试飞工程师深入理解燃油系统吸力供油试飞方法的内涵,根据被试对象及时对试飞方法做出优化。The flight test of aircraft fuel system involves many subjects. Based on the fluid mechanics theory and the GJB3212＂requirement of flight test for airplane fuel system＂,a theoretical explanation of the flight test method of suction fuel supply for aircraft fuel system is given. That helps other engineers to understand the flight test method of suction feed deeply and optimize the flight test method in time according to the subjects.

关 键 词：国军标 流体力学 吸力供油 飞行试验 

分 类 号：V217.1[航空宇航科学与技术—航空宇航推进理论与工程]