Numerical investigation of rotating cavitation in a three blade inducer

Engineering

• Room Temperature 100%
• Temperature Water 100%
• Liquid Oxygen 100%
• Radial Force 100%
• Flow Passage 50%
• Thermal Effect 50%
• Numerical Approach 50%
• Characteristic Frequency 50%
• Experimental Measurement 50%
• Cavitation Number 50%
• Blade Tip 50%
• Blade Surface 50%
• Inlet Pressure 50%
• Liquid Rocket Engine 50%
• Flow Rate Coefficient 50%