The response to vertical turbulence in cruise of the HTR XV-15 design is studied using simulation techniques. This design is a modified version of the XV-15 with a hingeless fiberglass soft-in-plane rotor system. The parameters of a gust alleviation system are determined and the performance of the system is evaluated over a range of cruise velocities and altitudes.
Simulation study of gust alleviation in a tilt rotor aircraft, volume 1
1977-06-01
Report
No indication
English
Adaptive Gust Alleviation for a Tilt-Rotor UAV Operating in Turbulent Airwakes
British Library Conference Proceedings | 2008
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