Using actuator disk analysis method, determine the requirement for a UAS to produce 8 lbf of thrust with an 8-inch prope
Posted: Tue Jun 07, 2022 5:45 pm
Using actuator disk analysis method, determine the requirement
for a UAS to produce 8 lbf of thrust with an 8-inch propeller in
BOTH hp and watts for altitudes of 0 to 5000 ft MSL in 1000 ft
increments with an equivalent airspeed of 25 knots across all
altitudes.
Show your results in a table.
for a UAS to produce 8 lbf of thrust with an 8-inch propeller in
BOTH hp and watts for altitudes of 0 to 5000 ft MSL in 1000 ft
increments with an equivalent airspeed of 25 knots across all
altitudes.
Show your results in a table.