[1] Mcnamara J J, Friedmann P P. Aeroelastic and aerothermoelastic analysis in hypersonic flow: past, present, and future. AIAA Journal, 2011, 49(6): 1089-1090.[2] Heeg J J, Gilbert M G, Pototzky A S. Active control of aerothermoelastic effects for a conceptual hypersonic aircraft. Journal of Aircraft, 1993, 30(4): 453-458.[3] Chavez F R, Schmidt D K. Analytical aeropropulsive/aeroelastic hypersonic-vehicle model with dynamic analysis. Journal of Guidance, Control, and Dynamics, 1994, 17(6): 1308-1319.[4] White D W, Huebner L D, Trexler C A, et al. Propulsion airframe integration test techniques for hypersonic air-breathing configurations at NASA Langley Research Center. AIAA-2003-4406, 2003.[5] Lind R, James R B, Andrew K S. Multi-loop aeroservoelastic control of a hypersonic vehicle. AIAA-1999-4123,1999.[6] Parker J T, Serrani A, Yurkovich S, et al. Control-oriented modeling of an air-breathing hypersonic vehicle. Journal of Guidance, Control, and Dynamics, 2007, 30(3): 856-869.[7] Clark A, Wu C, Mirmirani M, et al. Development of an airframe-propulsion integrated generic hypersonic vehicle model. AIAA-2006-218,2006.[8] Schmidt D K. Dynamics and control of hypersonic aeropropulsive/aeroelastic vehicles. AIAA-1992-4326, 1992.[9] Raney D L, McMinn J D, Pototzky A S, et al. Impact of aeroelasticity on propulsion and longitudinal flight dynamics of an air-breathing hypersonic vehicle. AIAA-1993-1367, 1993.[10] Xu Y. Studies on aeroelasticity of hypersonic vehicles. Beijing: School of Aeronautic Science and Engineering, Beihang University, 2008. (in Chinese) 许赟. 高超声速飞行器气动弹性问题研究. 北京: 北京航空航天大学航空科学与工程学院, 2008.[11] Chavez F R, Schmidt D K. Dynamics of hypersonic flight vehicles exhibiting significant aeroelastic and aeropropulsive interactions. AIAA-2003-7081, 2003.[12] Yang C, Wu Z G. Aeroservoelastic stability of missile. Flight Dynamics, 2000, 18(4): 1-5.(in Chinese) 杨超, 吴志刚. 导弹气动伺服弹性稳定性分析. 飞行力学, 2000, 18(4): 1-5. |