[1] Chen, S., Lyu, Z., Kenway, G.K.W., and Martins, J.R.R.A., “Aerodynamic Shape Optimization of Common Research Model, Wing–Body–Tail Configuration”, J. Aircraft, Vol. 53, No. 1, pp. 276-293, 2015.
[2] Castellani, M., Lemmens, Y., and Cooper, J.E., “Parametric Reduced Order Model Approach for Rapid Dynamic Loads Prediction”, Aerospace Sci. and Tech., Vol. 52, pp. 29-40, 2016.
[3] Ripepi, M., Verveld, M.J., Karcher, N.W., Franz, T., Abu-Zurayk, M., Görtz, S., and Kier, T.M., “Reduced-order Models for Aerodynamic Applications, loads and MDO”, CEAS Aeronautical Journal, Vol. 9, No. 1, pp. 171–193, 2018.
[4] Morton, S.A., Cummings, R.M., and Kholodar, D.B., “High Resolution Turbulence Treatment of F/A-18 Tail Buffet”, J. Aircraft, Vol. 44, No. 6, pp. 1769-1775, 2007.
[5] Attorni, A., Cavagna, L., and Quaranta, G., “Aircraft T-tail Flutter Predictions Using Computational Fluid Dynamics”, J. Fluids and Structures, Vol. 27, No. 2, pp. 161-174, 2011.
[6] Elham, A., La Rocca, G. and Vos, R., “Refined Preliminary Weight Estimation Tool for Airplane Wing and Tail”, SAE Technical Paper, 2011-01-2765, 2011.
[7] Decker, J.L., “Horizontal Tail Loads in Abrupt Pull-Ups from Level Flight”, J. the Aeronautical Sciences, Vol. 18, No. 12, pp. 835-841, 1951.
[8] Goron, G., Duca, R., Sarojini, D., Shah, S., Chakraborty, I., Briceno, S.I., and Mavris, D.N., “A Simulation-Based Framework for Structural Loads Assessment during Dynamic Maneuvers”, The 17th AIAA Aviation Tech., Integ., and Operations Conf., AIAA AVIATION Forum, (AIAA 2017-3767), 2017.
[9] Pearson, H.A., “Derivation of Charts for Determining the Horizontal Tail Load Variation with any Elevator Motion”, NASA ReportNo. 759, National Advisory Committee for Aeronautics, January 1943.