1. Vibration reduction in rotorcraft using active control - A comparison of various approaches
2. Rotary-Wing Aeroelasticity: Current Status and Future Trends
3. Key Results From a Higher Harmonic Control Aeroacoustic Rotor Test (HART)
4. 4Jacklin, S. A. “Second Test of a Helicopter Individual Blade Control System in the NASA Ames 40 by 80 Foot Wind Tunnel,” Proceedings of the 2nd International American Helicopter Society Aeromechanics Specialists Conference, Bridgeport, CT, Oct. 1995.
5. 5Jacklin, S. A., Haber, A., de Simone, G., Norman, T., Kitaplioglu, C., and Shinoda, P. “Full-Scale Wind Tunnel Test of an Individual Blade Control System for a UH-60 Helicopter,” Proceedings of the 51st Annual Forum of the American Helicopter Society, Montreal, Canada, June 2002.