Complexity / 2020 / Article / Fig 6

Research Article

Optimization of Fuel Injection Control System of Two-Stroke Aeroengine of UAV

Figure 6

Dynamic displacement of the needle valve with different spring initial tension F0. (a) F0 = 5.5 N. (b) F0 = 9.5 N. (c) F0 = 8.0 N.
(a)
(b)
(c)

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