[1] 张鲁民.航天飞机空气动力学分析[M].北京:国防工业出版社,2009.ZHANG L M.Aerodynamics analysis of space shuttle[M].Beijing:National Defence Industry Press,2009(in Chinese). [2] 蔡国飙,徐大军.高超声速飞行器技术[M].北京:科学出版社,2012.CAI G B,XU D J.Hypersonic vehicle technology[M].Beijing:Science Press,2012(in Chinese). [3] CHAUDHARY A,NGUYEN V,TRAN H,et al.Dynamics and stability and control characteristics of the X-37:AIAA-2001-4383[R].Reston:AIAA,2001. [4] GRANTZ A.X-37B orbital test vehicle and derivatives:AIAA-2011-7315[R].Reston:AIAA,2011. [5] 孙宗祥,唐志共,陈喜兰,等.X-37B的发展现状及空气动力技术综述[J].试验流体力学,2015,29(1):1-14.SUN Z X,TANG Z G,CHEN X L,et al.Review of the state-of-art and aerodynamic technology of X-37B[J].Journal of Experiments in Fluid Mechanics,2015,29(1):1-14(in Chinese). [6] 张庆.高速再入飞行器动力学问题研究[D].西安:西北工业大学,2018.ZHANG Q.Research on flight dynamics of high-velocity reentry vehicles[D].Xi'an:Northwestern Polytechnical University,2018(in Chinese). [7] 中国科学院.新型飞行器中的关键力学问题[M].北京:科学出版社,2018.Chinese Academy of Sciences.Key mechanical problems in new types of aircraft[M].Beijing:Science Press,2018(in Chinese). [8] 杨勇,张辉,郑宏涛.有翼高超声速再入飞行器气动设计难点问题[J].航空学报,2015,36(1):49-57.YANG Y,ZHANG H,ZHENG H T.Difficulties in aerodynamic design problems of the winged hypersonic reentry vehicle[J].Acta Aeronautica et Astronautica Sinica,2015,36(1):49-57(in Chinese). [9] 叶友达.高超声速空气动力学研究进展与趋势[J].科学通报,2015,60(12):1095-1103.YE Y D.Advances and prospects in hypersonic aerodynamics[J].Chinese Science Bulletin,2015,60(12):1095-1103(in Chinese). [10] 叶友达.高空高速飞行器气动特性研究[J].力学进展, 2009,39(4):387-397.YE Y D.Studies on aerodynamic characteristics of high velocity vehicle flying at high altitude[J].Advances in Mechanics,2009,39(4):387-397(in Chinese). [11] 庄逢甘, 赵梦熊.航天飞机的空气动力学问题[J].流体力学试验与测量,1987,1(4):1-8.ZHUANG F G,ZHAO M X.Aerodynamical problems of space shuttle[J].Experiments and Measurements in Fluid Dynamics,1987,1(4):1-8(in Chinese). [12] 蔡巧言,杜涛,朱广生.新型高超声速飞行器的气动设计技术探讨[J].宇航学报,2009,30(6):2086-2091.CAI Q Y,DU T,ZHU G S.The aerodynamic design technology for new type hypersonic vehicle[J].Journal of Astronautics,2009,30(6):2086-2091(in Chinese). [13] 蒋跃文.基于广义网格的CFD方法及其应用[D].西安:西北工业大学,2012.JIANG Y W.Numerical solution of Navier-Stokes equations on generalized mesh and its applications[D].Xi'an:Northwestern Polytechnical University,2012(in Chinese). [14] EAST R A,HUTT G R.Comparison of predictions and experimental data for hypersonic pitching motion stability[J].Journal of Spacecraft and Rockets,1988,25(3):225-233. [15] WELSH C J,WINCHENBACH G L,MADAGAN A N.Free-flight investigation of the aerodynamic characteristics of a cone at high mach numbers[J].AIAA Journal,1970,8(2):294-300. [16] BERTIN J J.Hypersonic aerothermodynamics[M].Reston:AIAA,1994. [17] 黄达,李志强,吴根兴.大振幅非定常试验数据表达与数学模型研究[J].空气动力学学报,1999,17(1):68-72.HUANG D,LI Z Q,WU G X.Study of data expression and mathematical modelling for unsteady experiment of a model pitching in large amplitude[J].Acta Aerodynamica Sinica,1999,17(1):68-72(in Chinese). [18] 刘绪,刘伟,柴振霞,等.飞行器动态稳定性参数计算方法研究进展[J].航空学报,2016,37(8):2348-2369.LIU X,LIU W,CHAI Z X,et al.Research progress of numerical method of dynamic stability derivatives of aircraft[J].Acta Aeronautica et Astronautica Sinica,2016,37(8):2348-2369(in Chinese). [19] LIU X,LIU W,ZHAO Y.Navier-Stokes predictions of dynamic stability derivatives for air-breathing hypersonic vehicle[J].Acta Astronautica,2016,118:262-285. [20] BRYAN G H, WILLIAMS W E.The longitudinal stability of aerial gliders[J].Proceedings of the Royal Society of London,1904,73:100-116. [21] ETKIN B, REID L D.Dynamics of flight:Stability and control[M].New York:Wiley,1996. [22] 张婉鑫,朱纪洪.大迎角非定常气动参数辨识研究[J].清华大学学报(自然科学版),2017,57(7):673-679.ZHANG W X,ZHU J H.Unsteady aerodynamic identification of aircraft at high angles of attack[J].Journal of Tsinghua University(Science & Technology),2017,57(7):673-679(in Chinese). [23] 黄达.飞行器大振幅运动非定常空气动力特性研究[D].南京:南京航空航天大学,2007.HUANG D.Unsteady aerodynamic characteristics for the aircraft oscillation in large amplitude[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2007(in Chinese). [24] 袁先旭,陈琦,谢昱飞,等.动导数数值预测中的相关问题[J].航空学报,2016,37(8):2385-2394.YUAN X X,CHEN Q,XIE Y F,et al.Problem in numerical prediction of dynamic stability derivatives[J].Acta Aeronautica et Astronautica Sinica,2016,37(8):2385-2394(in Chinese). |