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Hi
Tracy, I assume that the 15 degree limit is anywhere along the blade
rather than anyone radius. Is that correct? Best Guesses are
accepted :-)
TJ
Tracy Crook wrote:
That conclusion was based on measurements of the blade angle, prop rpm
& airspeed and calculating angle to airflow along with the assumption
that stall would occur when angle exceeded 15 deg. Then this SWAG was
boiled in a pot with observations of how adversely the cooling was
affected by the IVO (stalled air blocking inlets).
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