참고문헌
- Johnson, W., 1994, Helicopter Theory, Chap. 12, Dover Publications, Inc., N.Y.
- Newman, S., 1994, The Foundations of Helicopter Flight, Chap. 10, E. A., Great Britain.
- Roget, B., 2004, Individual Blade Control of Vibration Reduction of a Helicopter with Dissimilar Blades, Ph.D. Thesis, Chap. 1, Dept. of Aerospace Engineering, University of Maryland.
- Shin, S. -J., Cesnik, C. E. S. and Hall, S. R., 2007, Design and Simulation of Integral Twist Control for Helicopter Vibration Reduction, International Journal of Control, Automation, and Systems, Vol. 5, No. 1, pp. 24-34.
- Wilbur, M. L., Mirick, P. H., Yeager, W. T., Jr., Langston, C. W., Cesnik, C. E. S. and Shin, S. J., 2002, Vibratory Loads Reduction Testing of the NASA/Army/MIT Active Twist Rotor, Journal of the American Helicopter Society, Vol. 47, No. 2, pp. 123-133. https://doi.org/10.4050/JAHS.47.123
- Roth, D., Enenkl, B. and Dieterich, O., 2006, Active Rotor Control by Flaps for Vibration Reduction- Full Scale Demonstrator and First Flight Test Results, 32nd European Rotorcraft Forum, The Netherlands.
- Konstanzer, P., Enenkl, B., Aubourg, P.-A. and Cranga, P., 2008, Recent Advances in Eurocopter's Passive and Active Vibration Control, 64th AHS Annual Forum, Montreal, Canada.
- Straub, F., Anand, V., Birchette, T. and Lau, B., 2009, SMART Rotor Development and Wind-Tunnel Test, 35th European Rotorcraft Forum, Hamburg, Germany.
- Kottapalli, S., 2011, Enhanced Correlation of SMART Active Flap Rotor Loads, 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Denver, Colorado.
- Mainz, H., van der Wall, B. G., Leconte, P., Ternoy, F. and des Rochettes, H. M., 2005, ABC Rotor Blades: Design, Manufacturing and Testing, 31st European Rotorcraft Forum, Florence, Italy.
- Feszty, D., Nitzsche, F., Khomutov, K., Lynch, B. K., Mander, A. and Ulker, F. D., 2008, Design and Instrumentation of the SHARCS Scaled Rotor with Three Independent Control Systems, American Helicopter Society 64th Annual Forum, Montreal, Canada.
- Feszty, D. and Nitzsche, F., 2011, Review of Active Rotor Control Research in Canada, Int. Journal of Aeronautical and Space Sciences, Vol. 12, No. 2, pp. 93-114. https://doi.org/10.5139/IJASS.2011.12.2.93
- Balakumaran, N., Eun, W.-J., Lee, J.-H. and Shin, S.-J., 2012, Structural Design of an Active Trailing-Edge Flap Blade for Helicopter Vibration Control, Proceedings of the 53rd AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics and Materials Conference-Adaptive Structures Forum, Honolulu, Hawaii, USA.
- http://www.cedrat-technologies.com/(accessed 11/2012)
- Koratkar, N. A. and Chopra, I., 2002, Wind Tunnel Testing of a Smart Rotor Model with Trailing-edge Flaps, Journal of the American Helicopter Society, Vol. 47, No. 4, pp. 263-272. https://doi.org/10.4050/JAHS.47.263
- Clement, J. W., Brei, D. and Barrett, R., 1999, Wind Tunnel Testing of a High Authority Airspeed Insensitive Rotor Blade Flap, 40th AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, St. Louis, MO, USA.
- Prechtl, E. F., 2000, Design and Imple-mentation of a Piezoelectric Servo-flap Actuation System for Helicopter Rotor Individual Blade Control, Ph.D. Thesis, Chap. 4, Dept. of Aeronautics and Astronautics, MIT.
- http://www.mathworks.co.kr/kr/help/signal/ref/ tfestimate.html(accessed 02/2013)
- Laxman, V., Lim, J. H., Shin, S. J., Ko, K. H. and Jung, S. N., 2011, Power and Trim Estimation for Helicopter Sizing and Performance Analysis, Int'l Journal of Aeronautical and Space Science, Vol. 12, No. 2, pp. 156-162. https://doi.org/10.5139/IJASS.2011.12.2.156
- Koratkar, N. A. and Chopra, I., 1999, Design, Fabrication and Testing of a Mach Scaled Rotor Model with Trailing-Edge Flaps, American Helicopter Society 55th Annual Forum, Montreal, Canada.
- http://www.astbearings.com/product.html?product=F2-6 (accessed 11/2012)
- Lee, J.-H., Kim, T.-S. and Shin, S.-J., 2009, Design of an Intelligent Rotor with Flap for Vibration Reduction in Helicopters, Proceedings of the KSNVE Annual Spring Conference, pp. 460-461.
- Lee, J.-H., Choe, J.-H. and Shin, S.-J., 2011, Development of an Intelligent Active Trailing-edge Flap Rotor to Reduce Vibratory Loads in Helicopter, Proceedings of the KSNVE Annual Spring Conference pp. 492-497.
피인용 문헌
- Active Gurney Flap Design Modification for High Speed Operation and Natural Frequency Estimate vol.25, pp.10, 2015, https://doi.org/10.5050/KSNVE.2015.25.10.667