Numerical simulation of hybrid lubrication characteristics of slipper pair of aviation fuel piston pump

Engineering

• Aviation Fuels 100%
• Bottom Surface 33%
• Dynamic Pressure 100%
• Finite Volume Method 33%
• Inclination Angle 33%
• Inlet Pressure 33%
• Mathematical Model 66%
• Oil Film Thickness 66%
• Overturning Moment 33%
• Piston Pump 100%
• Pressure Distribution 33%
• Rotor Speed 33%
• Simulation Result 33%
• Static Pressure 100%