|Mar27-05, 07:46 PM||#1|
Thrust vs. Pressure Altitude
Greetings oh knowledgable ones,
I'm trying to figure out how to relate static thrust of a propeller driven recip to pressure altitude.
I know the higher you go the less air is supplied to the motor and therefore the less fuel can be mixed while retaining the max-power mixture.
I'm interested in a chart that might relate thrust (not HP - I have that) to pressure altitude.
Any help is appreciated!
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