Optimum Two-Per-Revolution Inputs for Improved Rotor Performance
Authors:
- 1 November 2005
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 42 (6) , 1409-1417
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Aerodynamic Analysis of a Helicopter in Steady Maneuvering Flight Using a Free-Vortex Rotor Wake ModelJournal of the American Helicopter Society, 1999
- Vibration reduction in rotorcraft using active control - A comparison of various approachesJournal of Guidance, Control, and Dynamics, 1995
- Forward flight trim and frequency response validation of a helicopter simulation modelJournal of Aircraft, 1993
- High‐Order State Space Simulation Models of Helicopter Flight MechanicsJournal of the American Helicopter Society, 1993
- Effects of higher harmonic control on rotor performance and control loadsJournal of Aircraft, 1992
- Theoretical Performance of Helicopters Having Second and Higher Harmonic Feathering ControlJournal of the American Helicopter Society, 1961
- Higher Harmonic Rotor ControlAircraft Engineering and Aerospace Technology, 1958