- #1
Badmachine
- 13
- 0
Is there a standard formula for determing the rate of change for an aircraft turn radius, while the aircraft angle of bank (AoB) is also changing? (from 0 degrees AoB - 40 degrees AoB during a turn for example)
Would aircraft speed play a role in the rate of change for the trun radius under these conditions?
Thanks
Would aircraft speed play a role in the rate of change for the trun radius under these conditions?
Thanks