linz2883 linz2883
  • 06-06-2023
  • Mathematics
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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.
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