https://bondline.org/index.php?action=history&feed=atom&title=File%3AO320_and_Propeller_Power_Curves.pngFile:O320 and Propeller Power Curves.png - Revision history2026-11-11T01:58:55ZRevision history for this page on the wikiMediaWiki 1.46.2https://bondline.org/index.php?title=File:O320_and_Propeller_Power_Curves.png&diff=2693&oldid=prevJbowman90: Shows the equilibrium points for a low and high compression O-320 and generic propeller performance roughly equivalent to a McCauley 7359, which is the cruise Cheetah propeller. Note the equilibrium brake horsepower increase for the same airspeed is well2008-01-21T16:05:21Z<p>Shows the equilibrium points for a low and high compression O-320 and generic propeller performance roughly equivalent to a McCauley 7359, which is the cruise Cheetah propeller. Note the equilibrium brake horsepower increase for the same airspeed is well</p>
<p><b>New page</b></p><div>Shows the equilibrium points for a low and high compression O-320 and generic propeller performance roughly equivalent to a McCauley 7359, which is the cruise Cheetah propeller. Note the equilibrium brake horsepower increase for the same airspeed is well in excess of the 6.7% from the engine only. Because of lower propeller efficiencies at higher RPMs, the thrust power improvement is not as high. The thrust power is the power used in various performance calculations.</div>Jbowman90