Ascending to cruise altitude at 400m


Liftoplane: ascending to cruise altitude at 400m RSI: ascending to cruise altitude at 400m

The time scaling is 1:10

During this operation, the rotors have a more decreased forward winding speed of about 12.8 m/s, consuming a power of 58.2 kW. The aircraft is not accelerating at all in any direction and has gained a horizontal speed of 50.68 m/s and a vertical speed of 5.79 m/s. Inflow dropped to 1.73 m/s. The aircraft operates like a lift going up at a speed of 9.85 m/s under a gliding wing with the equivalent LDR of 12.4. The propulsion efficiency increased to 99.47 percent. The aircraft is handled by using the biangular handling based on angles of attack with values of 6.0 and -0.2. The rotors have a PGS-state (1.0, -21.5, -10) with the decreased pitch, the reduced magnitude of the negative gain and the more inclined negative skew.



Getting cruise speed in ascent at 75m Ascending to cruise altitude at 3900m


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