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So the question that has been bugging me for about
a year is:
If we were to give up 10-15 knots could the IV be
made spin
resistant and or spin recoverable? It seems
like one or more
of the following might be true:
- h-stab/elevator not
effective in stall conditions
- rudder ditto
- effective washout is either
nil or negative
Has anyone looked at the aerodynamic
tradeoffs?
Colyn
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