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Thread: Turbojet - Thrust-producer /// Piston-prop - Power-producer
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Old 19th Mar 2013, 16:35
  #10 (permalink)  
hawk37
 
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A formula to convert horsepower to thrust assuming 100% propeller efficiency

THRUST = BHP*325/Velocity (knots)
How does that work Brian for a propellor aircraft at zero knots, engine run up ready for take off. Does your formula give infinite thrust?
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