I don not think that the KR can be landed full stall as the aoa
would have to be about 13 degrees. Hard to do with the tail
dragger configuration, Virg
On 2/15/2011 6:32 AM, PilotPond wrote:
> Could someone remind me what is the ideal angle the airplane should be
I wrote:
>Most KRs are around 10" (measured at the longeron).
That should have been "10 degrees (measured at the longeron)".
Apparently I'm getting too stupid to answer questions here anymore. Sleep
deprivation takes its toll eventually, at least that's my excuse, and I'm
sticking to it...
Ma
Darren wrote:
>>Could someone remind me what is the ideal angle the airplane should be at
when on the ground in tail dragger gear configuration? <<
Most KRs are around 10" (measured at the longeron). Obviously it would be
nice to be closer to stall angle, which is something like14 degrees to g
Could someone remind me what is the ideal angle the airplane should be at
when on the ground in tail dragger gear configuration?
My thinking is that during the landing you get a full stall of the wings
which if my limited understand of design is correct; should allow the
steerable tail wheel with
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