Gas Turbine Rotor Aerodynamics & Thermal Stress Visualizer

Blade Stage Velocity Triangles (Inlet V1, Relative W1, Speed U)

Absolute (V1)

Relative (W1)

Blade Speed (U)

Low Heat/Stress

Thermal Peak

Critical Root Shear

Blade Speed (U): 314.16 m/s

Isentropic Efficiency: 88.4%

Root Stress (MPa): 420.8 MPa

Power Output (MW): 340.5 MW

Operational Stage Presets

Kinematic & Flow Controls

Rotor RPM 3000 RPM

Blade Pitch Angle 28°

Inlet Temp (TIT) 1500 °C

Mass Flow Rate 650 kg/s

Calculated Aerodynamic Output

Blade Speed (U)

314.2 m/s

Isentropic Eff.

88.4%

Root Stress

420.8 MPa

Net Power

340.5 MW