The hover ceiling out of ground effect (OGE) is the maximum altitude at which an aircraft can hover without assistance from the ground. This altitude is influenced by various factors including engine power, air density, and weight of the aircraft.
P = Engine Power (Watts)
rho = Air Density (kg/mΒ³)
g = Acceleration due to Gravity (9.81 m/sΒ²)
C_T = Thrust Coefficient
The thrust coefficient (C_T) is a dimensionless parameter that depends on the aircraft’s design and operating conditions. It represents the ratio of thrust to power required for hovering.
What is hover ceiling OGE?
How do I calculate hover ceiling OGE?
What factors affect hover ceiling OGE?
Can I use this calculator for helicopters too?
What is the significance of the thrust coefficient (C_T)?
How does air density affect hover ceiling OGE?
Is ground effect considered in this calculation?
Results are for informational purposes only and do not constitute professional advice.
