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Old 21st February 2008 | 09:46
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infinity-it
 
Joined: Feb 2008
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From: Switzerland
Power Required Curve and Drag Polar for PA-34
I have to make a generic power required curve and a drag polar for a Piper Seneca-III (PA-34). The Seneca is equipped with a three blade prop.

Does anybody know where I can find the numbers like Oswald efficiency (e), Propeller efficiency (η), Zero lift drag coefficient (Cd0) and a table where I can find out the BHP for the Teledyne Continental TSIO-360KB engine at different altitudes?

Thank you very much for advise
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