참고문헌
- Anusonti-Inthra, P. and Gandhi, F. (2000). Helicopter vibration reduction through cyclic variations in rotor blade root stiffness. Journal of Intelligent Material Systems and Structures, 11, 153-166. https://doi.org/10.1106/B8NQ-4LNN-MPPL-AFHV
- Anusonti-Inthra, P. and Gandhi, F. (2001). Optimal control of helicopter vibration through cyclic variations in blade root stiffness. Smart Materials and Structures, 10, 86-95. https://doi.org/10.1088/0964-1726/10/1/308
- Bauchau, O. A. and Agarwal, S. (2006). The semi-active coulomb friction lead-lag damper concept. American Helicopter Society 62nd International Annual Forum Vol 3, Phoenix, AZ. pp. 1945-1953.
- Brassard, D. P. (2005). A 2D Transverse Vortex Wind Tunnel for PIV Invertigation of Airfoil Vortex Interaction. MS Thesis, Carleton University.
- Brigley, M., Welsh, W., Altieri, R., and Rich, A. (2011). Design and testing of a new vibration suppression system. American Helicopter Society 67th International Annual Forum, Virginia Beach, VA. Paper no. 163.
- Burwash, W. (2007). Particle Image Velocimetry Measurements of an Airfoil-Vortex Interaction Event in a Two- Dimensional Wind Tunnel. MS Thesis, Carleton University.
- Cesnik, C. E. S., Opoku, D. G., Nitzsche, F., and Cheng, T. (2004). Active twist rotor blade modelling using particlewake aerodynamics and geometrically exact beam structural dynamics. Journal of Fluids and Structures, 19, 651-668. https://doi.org/10.1016/j.jfluidstructs.2004.01.007
- Copp, P. and Chopra, I. (2008). Continued development of a mach scale swashplateless rotor with integrated trailing edge flaps. American Helicopter Society 64th International Annual Forum Vol 1, Montreal, QC. pp. 846-853.
- Coppotelli, G., Marzocca, P., Ulker, F. D., Campbell, J., and Nitzsche, F. (2008). Experimental investigation on modal signature of smart spring/helicopter blade system. Journal of Aircraft, 45, 1373-1380. https://doi.org/10.2514/1.35139
- Crozier, P., Leconte, P., Delrieux, Y., Gimonet, B., Le Pape, A., and des Rochettes, H. M. (2006). Wind-tunnel tests of a helicopter rotor with active flaps. Proceedings of the 32nd European Rotorcraft Forum, Maastricht, The Netherlands.
- Davis, G. L., Feszty, D., and Nitzsche, F. (2005). Trailing edge flow control for the mitigation of dynamic stall effects. Proceedings of the 31st European Rotorcraft Forum, Florence, Italy. pp. 53.1-53.11.
- Feszty, D., Gillies, E. A., and Vezza, M. (2004). Alleviation of airfoil dynamic stall moments via trailing-edge-flap flow control. AIAA Journal, 42, 17-25. https://doi.org/10.2514/1.853
- 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 International Annual Forum Vol 1, Montreal, QC. pp. 631-648.
- Feszty, D., Nitzsche, F., Mander, A., Coppotelli, G., Vetrano, F., Riemenschneider, J., and Wierach, P. (2009). Whirl tower demonstrations of the SHARCS hybrid control concept. American Helicopter Society 65th International Annual Forum, Grapevine, TX.
- Fuerst, D., Arnold, U. T. P., and Graham, D. (2011). In-flight tuning: wind tunnel test results and flight test preparations. American Helicopter Society 67th International Annual Forum, Virginia Beach, VA. Paper no. 359.
- Gennaretti, M., Poloni, L., and Nitzsche, F. (2003). 'Smart spring' identification for hovering rotor aeroelastic-stability augmentation. Aeronautical Journal, 107, 233-240.
- Gerontakos, P. and Lee, T. (2007). Trailing-edge flap control of dynamic pitching moment. AIAA Journal, 45, 1688-1694. https://doi.org/10.2514/1.27577
- Ghorashi, M. (2009). Dynamics of Elastic Nonlinear Rotating Composite Beams with Embedded Actuators. PhD Thesis, Carleton University.
- Ghorashi, M., Mikjaniec, T., Lynch, B., Ulker, F. D., Cha, M., Mander, A., Brassard, D. P., Feszty, D., and Nitzsche, F. (2006). Preliminary design of a scaled rotor blade with vibration and noise control devices. Proceedings of the 32nd European Rotorcraft Forum, Maastricht, The Netherlands. pp. 335-349.
- Ghorashi, M. and Nitzsche, F. (2008). Steady state nonlinear dynamic response of a composite rotor blade using implicit integration of intrinsic equations of a beam. International Review of Aerospace Engineering, 1, 225-233.
- Ghorashi, M. and Nitzsche, F. (2009). Nonlinear dynamic response of an accelerating composite rotor blade using perturbations. Journal of Mechanics of Materials and Structures, 4, 693-718. https://doi.org/10.2140/jomms.2009.4.693
- Gransden, D., Ghorashi, M., Langlois, R., and Nitzsche, F. (2005). Development of nonlinear elastic bending and torsion of articulated rotor blades with an impedance control device replacing the common pitch link. Proceedings of the 31st European Rotorcraft Forum, Florence, Italy. pp. 51.1-51.14.
- Hasegawa, Y., Katayama, N., Kobiki, N., Nakasato, E., Yamakawa, E., and Okawa, H. (2001). Experimental and analytical results of whirl tower test of ATIC full scale rotor system. American Helicopter Society 57th International Annual Forum, Washington, DC.
- Jacklin, S. A., Haber, A., de Simone, G., Norman, T. R., Kitaplioglu, C., and Shinoda, P. (2002). Full-scale wind tunnel test of an individual blade control system for a UH- 60 helicopter. American Helicopter Society 58th International Annual Forum, Montreal, QC.
- Khomutov, K. (2010). Design, Analysis and Instrumentation of the SHARCS Rotor Blade with Three Actively Controlled Systems. MS Thesis, Carleton University.
- Khoshlahjeh, M., Gandhi, F., and Webster, S. (2011). Extendable chord rotors for helicopter expansion and performance improvement. American Helicopter Society 67th International Annual Forum, Virginia Beach, VA.
- Kloeppel, V. and Enenkl, B. (2005). Rotor blade control by active helicopter servo flaps. International Forum on Aeroeleasticty and Structural Dynamics, Munich, Germany. Paper no. IF-158.
- Konstanzer, P., Enenkl, B., Aubourg, P. A., and Cranga, P. (2008). Recent advances in Eurocopter's passive and active vibration control. American Helicopter Society 64th International Annual Forum Vol 1, Montreal, QC. pp. 854- 871.
- Koratkar, N. A. and Chopra, I. (2001). Open-loop hover and wind tunnel testing of mach-scaled rotor with trailingedge flaps. 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Exhibit Technical Papers, Seattle, WA. pp. 1317-1331.
- Lorber, P., O'Neill, J., Hein, B., Isabella, B., Andrews, J., Brigley, M., Wong, J., and LeMasurier, P. (2011). Whirl and wind tunnel testing of the sikorsky active flap demonstrator rotor. American Helicopter Society 67th International Annual Forum, Virginia Beach, VA. Paper no. 041.
- Lynch, B., Ghorashi, M., and Nitzsche, F. (2005). On the use of shape memory alloy wires for anhedral angle control in helicopter rotor blades. 16th International Conference on Adaptive Structures and Technologies, Paris, France.
- Mander, A., Feszty, D., and Nitzsche, F. (2008). Active pitch link actuator for impedance control of helicopter vibration. American Helicopter Society 64th International Annual Forum Vol 2, Montreal, QC. pp. 1127-1137.
- Masaki, K., Hattori, K., Yoshimoto, M., Uchiyama, N., Nakao, M., Saito, S., and Kondo, N. (2005). Wind tunnel test for BVI noise and vibration reduction using blade active control. Proceedings of the 31st European Rotorcraft Forum, Florence, Italy. pp. 63.1-63.14.
- Maughmer, M., Lesieutre, G., and Kinzel, M. (2005). Miniature trailing-edge effectors for rotorcraft performance enhancement. American Helicopter Society 61st International Annual Forum, Grapevine, TX. pp. 1886-1897.
- McTavish, S. A. M. (2008). Advanced Aeroelastic Simulations for Practical Fixed-wing and Rotary-Wing Applications. MS Thesis, Carleton University.
- Mikjaniec, T. (2006). The Preliminary Design of the SHARCS Rotor Blade. MS Thesis, Carleton University.
- Muir, E. R., Liu, L., Friedmann, P. P., and Kumar, D. (2010). Hysteresis characterization in piezoceramic stack actuators and its influence on vibration and noise reduction in helicopters using actively controlled flaps. 51st AIAA/ ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Orlando, FL.
- Nitzsche, F. (1996). Smart spring-type actuation for helicopter individual blade control. Proceedings of the 6th International Conference on Adaptive Structures, Key West, FL. Paper no. 230-240.
- Nitzsche, F. and Breitbach, E. (1994). Vibration control of rotary wings using smart structures. Smart Materials and Structures, 3, 181-189. https://doi.org/10.1088/0964-1726/3/2/014
- Nitzsche, F. and Feszty, D. (2008). Hybrid Device for Vibration Control. US Patent no. 61/076,171, filed 27 (June 2008).
- Nitzsche, F., Feszty, D., Waechter, D., Bianchi, E., Voutsinas, S., Gennaretti, M., Coppotelli, G., and Ghiringhelli, G. L. (2005a). The SHARCS project: smart hybrid active rotor control system for noise and vibration attenuation of helicopter rotor blades. Proceedings of the 31st European Rotorcraft Forum, Florence, Italy. pp. 52.1-52.15.
- Nitzsche, F., Harold, T., Wickramasinghe, V. K., Yong, C., and Zimcik, D. G. (2005b). Development of a maximum energy extraction control for the Smart Spring. Journal of Intelligent Material Systems and Structures, 16, 1057-1066. https://doi.org/10.1177/1045389X05059964
- Nitzsche, F., Lammering, R., and Breitbach, E. (1993). Can smart materials modify blade root boundary conditions to attenuate helicopter vibration? Proceedings of the 4th International Conference on Adaptive Structures, Cologne, Germany. pp. 139-150.
- Nitzsche, F. and Opoku, D. G. (2005). Acoustic validation of a new code using particle wake aerodynamics and geometrically-exact beam structural dynamics. Aeronautical Journal, 109, 257-267. https://doi.org/10.1017/S0001924000000713
- Opoku, D. G. (2002). Aeroelastic and Aeroacoustic Modelling of Rotorcraft. MS Thesis, Carleton University.
- Oxley, G. (2009). A 2-D Hybrid Euler-Compressible Vortex Particle Method for Transonic Rotorcraft Flows. PhD Thesis, Carleton University.
- Oxley, G., Nitzsche, F., and Feszty, D. (2009). Smart spring control of vibration on helicopter rotor blades. Journal of Aircraft, 46, 692-696. https://doi.org/10.2514/1.27914
- Park, J. S., Kim, S. H., Jung, S. N., and Lee, M. K. (2011). Design and analysis of variable-twist tiltrotor blades using shape memory alloy hybrid composites. Smart Materials and Structures, 20(1).
- Richardson, M., Feszty, D., A., P. J., Nitzsche, F., Khomutov, K. V., Vamosi, S. B., and Young, R. D. (2011). Towards closedloop control tests of the SHARCS active pitch link in the rotating frame. American Helicopter Society 67th International Annual Forum, Virginia Beach, VA. Paper no. 274.
- Riemenschneider, J., Keye, S., Wierach, P., and Mercier Des Rochettes, H. (2005). Review of the common DLR/ONERA project "Active Twist Blade" (ATB). Proceedings of the 30th European Rotorcraft Forum, Marseilles, France. pp. 273-281.
- Roth, D., Enenkl, B., and Dieterich, O. (2007). Active rotor control by flaps for vibration reduction-full scale demonstrator and first flight test results. Proceedings of the 32nd European Rotorcraft Forum, Maastricht, The Netherlands. pp. 801-814.
- Schimke, D., Arnold, U. T. P., and Kube, R. (1998). Individual blade root control demonstration evaluation of recent flight tests. American Helicopter Society 54th International Annual Forum Vol 1, Washington, DC. pp. 378-390.
- Schlegel, R., King, R., and Mull, H. (1996). Helicopter Rotor Noise Generation and Propagation. USAAVLABS Technical Report 66-4. Virginia, VA: US Army Aviation Materiel Laboratories.
- Schmidt, D. A. (2010). A Systematic Study Of Airfoil-Vortex Interactions by Means of Particle Image Velocimetry. MS Thesis, Carleton University.
- Splettstoesser, W. R. (1993). The HELINOISE Aeroacoustic Rotor Test in the DNW: Test Documentation and Representative Results. DLR-Mitt. 93-09. Braunschweig: Institut fur Entwurfsaerodynamik DLR.
- Stepniewski, W. Z. and Keys, C. N. (1984). Rotary-Wing Aerodynamics. Vol. II: Performance Prediction of Helicopters. New York: Dover Publications. pp. 103-104.
- Straub, F. K., Anand, V. R., Birchette, T. S., and Lau, B. H. (2009). Smart rotor development and wind tunnel test. Proceedings of the 35th European Rotorcraft Forum, Hamburg, Germany. pp. 413-430.
- Straub, F. K., Kennedy, D. K., Stemple, A. D., Anand, V. R., and Birchette, T. S. (2004). Development and whirl tower test of the SMART active flap rotor. Proceedings of the SPIE, 5388, 202-212. https://doi.org/10.1117/12.562645
- Thepvongs, S., Cook, J. R., Cesnik, C. E. S., and Smith, M. J. (2009). Computational aeroelasticity of rotating wings with deformable airfoils. American Helicopter Society 65th International Annual Forum Vol 1, Grapevine, TX. pp. 790- 805.
- Ulker, F. D. (2011). A New Framework for Helicopter Vibration Suppression: Time-Periodic Identification and Controller Design. PhD Thesis, Carleton University.
- Ulker, F. D., Mander, A., Feszty, D., and Nitzsche, F. (2008). SHARCS: Hybmd control concept for vibration reduction of helicopters. Proceedings of the 34th European Rotorcraft Forum, Liverpool, UK. pp. 2020-2052.
- Vallejo, P., Lopez, J., Rios-Tejada, F., Azofia, J., Del Valle, J., Velasco, C., and Garcia-Mora, L. (1998). Low back pain in helicopter pilots. RTO HFM Symposium on Current Aeromedical Issues in Rotary Wing Operations, San Diego, CA.
- Voutsinas, S. G. (2006). Vortex methods in aeronautics: How to make things work. International Journal of Computational Fluid Dynamics, 20, 3-18. https://doi.org/10.1080/10618560600566059
- Wall, A. S., Afagh, F. F., Langlois, R. G., and Zan, S. J. (2008). Modeling helicopter blade sailing: dynamic formulation and validation. Journal of Applied Mechanics, 75, 061004. https://doi.org/10.1115/1.2957599
- Wierach, P., Riemenschneider, J., Optiz, S., and Hoffmann, F. (2007). Experimental investigation of an active twist model rotor blade under centrifugal loads. Proceedings of the 33rd European Rotorcraft Forum, Kazan, Russia. pp. 1653-1665.
- Wilbur, M. L., Mirick, P. H., Yeager Jr, W. T., Langston, C. W., Cesnik, C. E. S., and Shin, S. (2002). Vibratory loads reduction testing of the NASA/Army/MIT active twist rotor. Journal of the American Helicopter Society, 47, 123-133. https://doi.org/10.4050/JAHS.47.123
- Wilkins, J. (2005). Commissioning and Calibration of the Carleton University High Sub-Sonic 2-D Blade Vortex Interaction Investigation. MEng Project Report. Ottawa, ON: Carleton University.
- Woods, B. K. S., Choi, Y. T., Wereley, N. M., and Kothera, C. S. (2011). Control system development for pneumatic artificial muscle driven active rotor systems. American Helicopter Society 67th International Annual Forum, Virginia Beach, VA.
피인용 문헌
- Enhancement of SNUF Active Trailing-edge Flap Blade Mechanism Design vol.23, pp.7, 2013, https://doi.org/10.5050/KSNVE.2013.23.7.645
- Design of the propelling nozzles for the launchers and satellites vol.15, pp.1, 2014, https://doi.org/10.5139/IJASS.2014.15.1.91