Explains the origins of rotor aerodynamic limits for helicopters including retreating and advancing blade limits. Examines the compounding of a helicopter for higher forward speed and reports the conclusions of a student project to design a rotorcraft capable of 300 knots and carrying a payload of 30 passengers.
Aircraft Engineering and Aerospace Technology – Emerald Publishing
Published: Oct 1, 1997
Keywords: Aerospace engineering; Design; Tests
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