27 Toward Active Control of Limit Cycle Oscillations in an Aeroelastic Wing. . . 213 Funding Sources Funding for this research is provided by the National Science Foundation for its financial support of this study under Award No. CMMI-2015983, which is managed by Dr. Robert Landers. References 1. Garrick, I.E., Reed, W.H.: Historical development of aircraft flutter. J. Aircr. 18(11), 897–912 (1981) 2. Ricketts, R.H.: Experimental aeroelasticity history, status and future in brief, NASA Technical Report, TM-102651, April 1990 3. Theodorsen, T.: General theory of aerodynamic instability and the mechanism of Flutter, Tech. Rep. 496, NACA, 1935 4. Patil, M.J., Hodges, D.H.: On the importance of aerodynamic and structural geometrical nonlinearities in aeroelastic behavior of high-aspectratio wings. J. Fluids Struct. 19 , 905–915 (2004) 5. O’Neil, T., Gilliatt, H., Strganac, T.W.: Investigations of aeroelastic response for a system with continuous structural nonlinearities. Proc. AIAA 37th structure, structural dynamics and materials, April 1996 6. Goodman, C., Hood, M., Reichenbach, E., Yurkovich, R.: An analysis of the F/A-18C/D Limit cycle oscillation solution. 44th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference, 2003 7. Hayes, W.B., Sisk, K.: Prevention of External Store Limit Cycle Oscillations on the F/A-18E/F Super Hornet and EA-18G Growler Aircraft.,” Tech. Rep. RTO-MP-AVT-152,. North Atlantic Treaty Organization/Science and Technology Organization (2008) 8. Dowell, E.H., Tang, D.: Nonlinear aeroelasticity and unsteady aerodynamics. AIAA J. 40(9), 1697–1707 (2002) 9. Pidaparthi, B., Missoum, S.: Stochastic optimization of nonlinear energy sinks for the mitigation of limit cycle oscillations. AIAA J. 57(5) , 2134–2144 (2019) 10. Bichiou, Y., Hajj, M.R.: Effectiveness of a nonlinear energy sink in the control of an aeroelastic system. Nonlinear Dynamics. 86 , 2161–2177 (2016 ) 11. Strganac, T.W., Ko, J., Thompson, D.E., Kurdila, A.J.: Identification and control of limit cycle oscillations in aeroelastic systems. J. Guid. Control. Dyn. 23(6), 1127–1133 (2000) 12. Bryant, M., Garcia E.: Development of an aeroelastic vibration power harvester. Proc. SPIE 7288, active and passive smart structures and integrated systems, April 2009 13. Bryant, M., Garcia E.: Energy harvesting: a key to wireless sensor nodes. Proc. 7493, Second international conference on smart materials and nanotechnology in engineering, Oct 2009 14. Zhao, L., Yang, Y.: Enhanced aeroelastic energy harvesting with a beam stiffener. Smart Mater. Struct. 24(3), 032001 (2015) 15. Kirschmeier, B., Bryant, M.: Experimental investigation of wake-induced aeroelastic limit cycle oscillations in tandem wings. J. Fluids Struct. 81 , 309–324 (2018) 16. Gianikos, Z.N., Kirschmeier, B.A., Gopalarathnam, A., Bryant, M.: Limit cycle characterization of an aeroleastic wing in a bluff body wake. J. Fluids Struct. 95 , 102986 (2020) 17. Kirschmeier, B.A., Gianikos, Z., Gopalarathnam, A., Bryant, M.: Amplitude annihilation in wake-influenced aeroelastic limit-cycle oscillations. AIAA J. 58(9), 4117–4127 (2020) 18. Visbal, M.R., Garmann, D.J.: Numerical investigation of Spanwise end effects on dynamic stall of a pitching NACA 0012 Wing. Proc. 55th AIAA aerospace sciences meeting, Jan 2017 19. Rockwood, M., Medina, A.: Controlled generation of periodic vortical gusts by the rotational oscillation of a circular cylinder and attached plate. Exp. Fluids. 61(3), 65 (2020) 20. Chen, Y., Zhang, S., Zhang, W., Peng, J., Cai, Y.: Multifactor spatio-temporal correlation model based on a combination of convolutional neural network and long short-term memory neural network for wind speed forecasting. Energy Convers. Manag. 185 , 783–799 (2019)
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