vertical versus airspeed
Erik,
I determined the vertical height in a hammer head versus entrance airspeed awhile back, but can't find the data. Aircraft is an RV-4, 160 hp, fixed Performance prop, max rpm 2750 WOT, entrance altitude 2000 feet AGL, 4 G pull to vertical. Airspeeds varied from 110 to 160 knots. The max vertical at the top of the hammer head was about 1100 feet at 160 knots rotation speed. I also saw 7000 ft/min on the VS with the Dynon.
Cheers,
Bill McLean
RV-4 slider
Alabama (roll tide)