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0 reviewsThis thesis focuses on studying system- and component-level phenomena in the fighter aircraft hydraulic power supply system in detail. The objective is to find out system-level root causes for premature failures of hydraulic pumps encountered in many modern fighter aircraft, and to study phenomena related to them. The thesis establishes a theoretically justified basis for understanding the interactions of the hydraulic system, bootstrap-type reservoir and axial piston hydraulic pump. It also presents a cost-effective and flexible method for studying system- and componentlevel phenomena in an aircraft hydraulic system by combining a theoretical approach with ground and laboratory testing.
