Hi, this is steady-state CFD simulation report of:

tcfdcase0

Created by TCFD^® 19.10 on Wed Jan 22 14:14:16 2020

Simulation Stats

Test Case Name

tcfdcase0

Number of Points [ – ]

Machine Type

propeller

Rotation Speed [ RPM ]

8000.00

Number of Components [ – ]

( )

Mesh Size [ cells ]

( )

Domain : 290349

Rotor : 217328

Total : 507677

Average y+ at walls [ – ]
( )

Wall-clock time [ hh:mm:ss ]

00:13:03

Parallel Processors [ – ]

Fluid Name

air

Physical Model

incompressible

Equation of state

Numerical order

first

Turbulence model

kOmegaSST

Performance Curve

2:rotor-inlet — 2:rotor-freestream,2:rotor-outlet

Point Nr.	Advance Ratio [ – ]	Thrust Coefficient [ – ]	Torque Coefficient [ – ]
1	0.255508	0.0961792	0.0198722

Efficiency

2:rotor-inlet — 2:rotor-freestream,2:rotor-outlet

Point Nr.	Velocity Magnitude [ m/s ]	Efficiency [ – ]
1	4.32660	0.196816

Torque

Point Nr.	Torque [ N.m ]
1	0.0140063

Axial Force

Point Nr.	Axial Force [ N ]
1	0.533771

Force Coefficients

#1: 2:propeller-LETE, 2:propeller-PS, 2:propeller-SS, 2:propeller-hub

Setup Nr.	Point Nr.	Lift Coeff [ – ]	Drag Coeff [ – ]	Moment Coeff [ – ]
1	1	-0.889618	2.76083 × 10^-5	0.0233438

Forces X Y Z

#1: 2:propeller-LETE, 2:propeller-PS, 2:propeller-SS, 2:propeller-hub

Setup Nr.	Point Nr.	Fx [ N ]	Fy [ N ]	Fz [ N ]
1	1	1.65650 × 10^-5	-0.533771	2.46710 × 10^-4

Torques X Y Z

#1: 2:propeller-LETE, 2:propeller-PS, 2:propeller-SS, 2:propeller-hub

Setup Nr.	Point Nr.	Tx [ N.m ]	Ty [ N.m ]	Tz [ N.m ]
1	1	4.53065 × 10^-6	0.0140063	-3.77194 × 10^-5

Design: HTML5 UP

TCFD^® 19.10 license is issued for CFDSUPPORT Test Licence as Limited and will be valid until Oct 06, 2022.