joema
20th Sep 2011, 19:17
I've seen Sean Tucker's Oracle biplane *apparently* hover, or nearly so. It has a hp-to-weight ratio of about 1:3, or 3 lbs per hp.
High powered corporate turboprops like the Cheyenne 400LS when lightly loaded start to approach that hp-to-weight ratio, maybe 4.5 lbs per hp (better than a P-51 Mustang).
Is there some rule of thumb for hp-to-weight ratio required to theoretically hover in a 90 deg. AOA for a fixed-wing propeller aircraft at sea level on a standard day?
High powered corporate turboprops like the Cheyenne 400LS when lightly loaded start to approach that hp-to-weight ratio, maybe 4.5 lbs per hp (better than a P-51 Mustang).
Is there some rule of thumb for hp-to-weight ratio required to theoretically hover in a 90 deg. AOA for a fixed-wing propeller aircraft at sea level on a standard day?