Does anybody know if ground effect lowers your stall speed?

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I always believed that it did not, so I was surprised to read the
compelling evidence from John M, viz., "Mine actually lifts off at 37
knots in ground effect and will fly a foot or so above the ground
however stall at altitude is at about 42 knots".

I suspect that the TAS does not change, but the IAS does due to the
ground effect on airflow around the pitot.  Would be interesting to hear
from the KR that has the pitot on top of the Fin.

For your purposes right now, I guess the best answer is yes - what you
will see on the ASI will be lower in ground effect (compared to readings
observed at altitude).

What have you decided regarding the canopy latch and the turtle deck
attachments?

Good luck

Steve J



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