Originally posted by eskimo2
Believe it or not, the traction requirements for this scenario are no greater than the traction needed to hold a plane on a tarmac with its engines on full power and it brakes on full – locked.
Is that why ball in second film doesn't stick to your belt (paper, fabric or whatever it is)?
Why don't you calculate real world example, a small plane like Cessna 172?
Here, some data to start with:
# Length: 27 ft 2 in (8.28 m)
# Wingspan: 36 ft 1 in (11.0 m)
# Height: 8 ft 11 in (2.72 m)
# Wing area: 174 ft² (16.2 m²)
# Airfoil: NACA 2412 (modified)
# Empty weight: 1,620 lb (736 kg)
# Useful load: 830 lb (376 kg)
# Max takeoff weight: 2,450 lb (1,113 kg)
# Powerplant: 1× Lycoming IO-360-L2A flat-4 engine, 160 hp (120 kW) at 2,400 rpm
# * Zero-lift drag coefficient: 0.0319
# Drag area: 5.58 ft² (0.52 m²)
# Aspect ratio: 7.32
# Lift-to-drag ratio: 11.6
# Wing loading: 14.1 lb/ft² (68.8 kg/m²)
# Power/mass: 15.3 lb/hp (9.25 kg/kW)
Of course, you can chose other type, maybe jet, so you'll know amount of thrust for certain.
Let us know when you have results, I'll be happy to check them out and admit defeat if it turns out that way.
Heck I'll even say you were right about your triplets.
Until then I'm out of this thread.
