Dynamic Hydraulic System Simulation-An Integrated Approach
902003
09/01/1990
- Event
- Content
- This paper describes a dynamic aircraft hydraulic system simulator model. This model uses a flexible approach that accounts for flight control loads, system stiffness, line losses, internal leakage at individual valve packages, pump compensator response, and power input to engine-driven pumps at various engine rpm. The model integrates performance of the flight controls, hydraulics, and power sources allowing accurate simulation of the airplane.
- Pages
- 12
- Citation
- Bang, B., and Draxler, J., "Dynamic Hydraulic System Simulation-An Integrated Approach," SAE Technical Paper 902003, 1990, https://doi.org/10.4271/902003.