We can build or buy a propeller that is 5 feet in diameter and that has a maximum efficiency of 93% when it is operating at an Advance Ratio of 1.35. The engine we are using to drive the propeller provides optimum torque and fuel economy when turning at a shaft speed of 3000 RPM.
Optimum aircraft airspeed (in knots) for this propeller/engine combination is 337.5 ft/sec.
Mach Number at the propeller’s tip when operating at optimum RPM and airspeed at sea level standard day conditions is 2.492.
Help Please!!!!!!!!!!!!!!!!!!
Find the shaft horsepower required of the engine if the total aircraft drag at the optimum condition above is 500 pounds.
2007-04-17
08:07:06
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2 answers
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Science & Mathematics
➔ Engineering