
Blade-element momentum analysis using the propeller’s geometry and section aerodynamics.
Includes model-level quantities; saved results vary by analysis mode.
Performance
- Rotational speed · RPM / Hz
- Thrust · N
- Aerodynamic torque · N·m
- Aerodynamic power · W
- Advance ratio · J
- Thrust coefficient · Cₜ
- Power coefficient · Cₚ
- Propulsive efficiency · η / Pe
- Induced efficiency
- Profile efficiency
- Tip Mach number
- Representative Reynolds number
- Exit velocity · m/s
- Thrust-to-power ratio
Blade stations
Radial analysis
- Station index, radius and r/R
- Chord and twist
- Angle of attack · °
- Reynolds and Mach numbers
- Lift and drag coefficients · CL / CD
- Axial velocity · m/s
- Tangential velocity · m/s
- Relative air velocity · m/s
- Induced axial velocity · m/s
- Induced swirl velocity · m/s
- Section thrust contribution · N
- Section torque contribution · N·m
- Stall angle · °
- Flow separation
Oblique and transient flow
When enabled
- Axial and edgewise inflow · m/s
- In-plane force · N
- Ground-frame vertical and horizontal force · N
- Induction scale
- Uniform and two harmonic inflow states
Diagnostics
- Blade-solve convergence
- Fraction above critical Mach
- Fraction above drag-divergence Mach
- Compressibility warning
- Inflow validity / vortex-ring-state flag
- Raw thrust and power coefficients
- Validation-envelope status and limiting factor








