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#30
04-26-2011, 08:33 PM
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However, once the aeroplane is flying, the tip speed is
((static tip speed)^2+TAS^2)^0.5 So at say 150 m/s TAS your static 222 m/s tip speed becomes more like 268 m/s. At 20,000 feet this is a Mach number of about 0.85. 
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