Bramwell's Helicopter Dynamics 2000
DOI: 10.1016/b978-075065075-5/50009-9
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Totor aerodynamics in forward flight

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“…Of course, the propeller thrust line is not the only means of producing pitching moments. A rotor system with offset flapping hinges will produce a moment that is independent of rotor thrust, but proportional to flap angle* 16 ). Since the gyroplane rotor will be flapped back relative to the fuselage to provide the requisite axial flow for autorotative flight, appropriate choice of mast angle will result in a nose-up moment with this type of rotor system, which will be balanced by placing the thrust line aft of the centre-ofmass.…”
Section: M">0mentioning
confidence: 99%
“…Of course, the propeller thrust line is not the only means of producing pitching moments. A rotor system with offset flapping hinges will produce a moment that is independent of rotor thrust, but proportional to flap angle* 16 ). Since the gyroplane rotor will be flapped back relative to the fuselage to provide the requisite axial flow for autorotative flight, appropriate choice of mast angle will result in a nose-up moment with this type of rotor system, which will be balanced by placing the thrust line aft of the centre-ofmass.…”
Section: M">0mentioning
confidence: 99%