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Forum: Tech Log
14th Mar 2011, 20:07
Replies: 43
Views: 27,375
Posted By willl05

Is it possible that the formula for TAS is wrong?

Or maybe the explanation in 1.11.1 is wrong:

VKTAS = VKIAS × [1+ (altitude× 0.00002)]
Where V = Indicated Airspeed
altitude = Maximum segment altitude in thousands of feet

For 200 knots at...
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