Post by Br. Marius on Feb 13, 2015 18:51:35 GMT
For a speed of 200 ft/sec, calculate the rotor control angles (collective θ0, lateral cyclic θ1c, and longitudinal cyclic θ1s) required to produce a thrust of 300 lbs, and zero first harmonic flapping, i.e. β1s and β1c = 0.