Effect of radial location of nozzles on performance of preswirl systems: a computational and theoretical study

Engineering

• Discharge Coefficient 100%
• Theoretical Study 100%
• Rotors 66%
• Swirl Ratio 66%
• Flowrates 66%
• Simple Model 33%
• Inlet Nozzle 33%
• Flow Structure 33%
• Rotational Reynolds Number 33%
• Good Agreement 33%
• Flow Parameters 33%
• Analytical Result 33%
• Gas Turbine 33%
• Experimental Result 33%
• Turbulent Flow 33%
• Rotating Core 33%
• Performance Parameter 33%
• Reynolds-Averaged Navier-Stokes 33%
• Steady-State Model 33%
• Show Value 33%
• High Reynolds Number 33%
• Engine Designer 33%
• Stator System 33%
• Navier-Stokes Equation 33%
• Scale Model 33%