Iplayfarmer said:
Pat,
I don't think anyone is trying to say that ground effect causes a stall.
I've been trying to say what you're saying... the lack of ground effect is what facilitates the stall. I.e. "after reaching the upper limit of the ground effect which had been aiding his climb".
Perhaps I was led astray by the following I reproduced from earlier posts, assertions that are not entirely true:
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"So... Ground effect will only come into play if the plane is overloaded, at which point the plane will take off due to ground effect and then stall crashing into Eddie's lake truly scaring whatever fish haven't been liquified by the magic impeller causing the backwards current.
Once the pilot climbs out of ground effect wingtip vortices will form, the wings will stall, and the aircraft will suddenly descend - usually resulting in a crash."
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Many modern aircraft have special wingtips that induce a rotating component to be equal in magnitude and opposite in phase (direction) to wing tip vortices and cancel them over a relatively wide dynamic range of aerodynamic conditions, especially but not restricted to cruise configuration.
A crash is only probable if 1. the pilot does what I described earlier, try to maintain the ground effect assisted rate of climb. Pilots can get nervous when during a takeoff-climbout their VSI swings to less positive numbers or negative values. If they make the error of flying the VSI as a control instrument rather than as intended, a performance instrument, they can easily achieve a greater angle of attack than can be maintained, lose lift, and approach or enter a stall condition.
or 2. (a variant of the above) the pilot sets up an unrealistically rapid ascent after rotation and lift off (relatively easily achieved with ground effect) and gets well above the altitude where ground effect would cushion him sufficiently and after having traded off airspeed for altitude (kinetic energy for potential energy) rapidly finds himself too nose high and too low on airspeed with an ensuing stall.
With conventional (old fashioned original recipe wings) both of the above scenarios is more likely but not assured.
Note: a stall in and of itself is not dangerous to the aircraft or occupants but requires the loss of altitude for a recovery Iin "normal aircraft" and when the required loss of altitude exceeds the height above solid objects of the aircraft a lot of impromptu customizing of the airframe and the pilot's frame is likely.
Note2: If the climb after rotation is more gradual, the overweight (for available power) aircraft will gently be trapped near the top of the ground effect with no stall. It would still be a frightening thing to be flying cross country at an elevation of (say) 50-80 feet (depending on the wing loading, power available, etc.
Since the magic impeller will prevent the float plane from taking off or even moving forward, all the discussion regarding ground effect is, although of some passing interest, not applicable to the problem at hand.
Pat