Acknowledgement
본 연구는 국방과학연구소의 지원으로 차세대 고속 복합형 무인 회전익기 특화연구실에서 수행되었습니다.
References
- A. J. Ruddell, "Advancing Blade Concept(ABC) Technology Demonstrator," U. S. Army Research and Technology Laboratories, USAAVRADCOM-TR-81-D-5, April, 1981.
- Y.-M. Kwon, J.-S. Park, "Performance and Airloads Analyses for a Rigid Coaxial Rotor of High-Speed Compound Unmanned Rotorcrafts," Journal of the Korea Institute of Military Science and Technology, Vol. 23, No. 4, pp. 311-318, 2020. https://doi.org/10.9766/KIMST.2020.23.4.311
- A. Bagai, "Aerodynamic Design of the X2 Technology DemonstratorTM Main Rotor Blades," 64th American Helicopter Society International Annual Forum, 2008.
- Y.-M. Kwon, J.-S. Park, S.-Y. Wie, H. J. Kang, D.-H. Kim, "Aeromechanics Analyses of a Modern Lift-Offset Coaxial Rotor in High-Speed Forward Flight," International Journal of Aeronautical and Space Sciences, Vol. 22, No. 2, pp. 338-351, 2021. https://doi.org/10.1007/s42405-020-00300-8
- J. O'Leary, W. Miao, "Design of Higher Harmonic Control for the ABCTM," Journal of the American Helicopter Society, Vol. 27, No. 1, pp. 52-57, 1982. https://doi.org/10.4050/JAHS.27.52
- W. Johnson, "CAMRAD II: Comprehensive Analytical Method of Rotorcraft Aerodynamics and Dynamics," Johnson Aeronautics, Palo alto, CA, USA, 2012.
- S.-B. Hong, Y.-L. Lee, Y.-M. Kwon, J.-S. Park, J.-S. Kim, "Airframe Vibration Reduction for an Unmanned Lift-Offset Compound Helicopter Using Active Vibration Control System," Shock and Vibration, Under Review, 2021.
- M. Hashemi-Kia, M. Toossi, "Development and Application of a Technique for Reducing Airframe Finite Element Models for Dynamics Analysis," NASA CR 187448, October, 1990.
- Y.-L. Lee, D.-H. Kim, J.-S. Park, S.-B. Hong, "Vibration Reduction Simulations of a Lift-Offset Compound Helicopter Using Two Active Control Techniques," Aerospace Science and Technology, Vol. 106, Article 106181, 2020.