[1] 占云.超燃冲压发动机的第一个40年[J].飞航导弹,2002(9):32-40.ZHAN Y.Scramjet's first 40 years[J].Winged Missiles Journal,2002(9):32-40(in Chinese). [2] 王巍巍,郭琦.美国典型的高超声速技术研究计划(上)[J].燃气涡轮试验与研究,2013,26(3):53-58.WANG W W,GUO Q.Typical hypersonic technology research programs in America (PartⅠ)[J].Gas Turbine Experiment and Research,2013,26(3):53-58(in Chinese). [3] PEEBLES C.Road to Mach 10:Lessons learn from the X-43A flight research program[M].Reston:AIAA,2008:36-78. [4] SHELLY F,CHARLES M,KENNETH R,et al.Hyper-X Mach 7 scramjet design,ground test and flight result:AIAA-2005-3322[R].Reston:AIAA,2005. [5] 甄华萍,蒋崇文.高超声速技术验证飞行器HTV-2综述[J].飞航导弹,2013(6):7-13.ZHEN H P,JIANG C W.Overview of hypersonic technology verification vehicle HTV-2[J].Winged Missiles Journal,2013(6):7-13(in Chinese). [6] PHILLIPS W H.Effect of rolling on longitudinal and directional stability:NASA TN-1627[R].Washington,D.C.:NASA,1948. [7] MEHRA R K,CARROLL J V.Bifurcation analysis of aircraft high angle-of-attack flight dynamics:AIAA-1980-1599[R].Reston:AIAA,1980. [8] KANDIL O A,MENZIES M A.Effective control of simulated wing rock in subsonic flow:AIAA-1997-0831[R].Reston:AIAA,1997. [9] LIU W,ZHANG H X,ZHAO H Y.Numerical simulation and physical characteristics analysis for slender wing rock[J].Journal of Aircraft,2006,43(3):858-861. [10] 杨小亮,刘伟,赵云飞,等.80°后掠三角翼强迫俯仰、自由滚转双自由度耦合运动特性数值研究[J].空气动力学学报,2011,29(4):421-426.YANG X L,LIU W,ZHAO Y F,et al.Numerical investigation of the characteristics of double degree-of-freedom motion of an 80° delta wing in force-pitch and free-roll[J].Acta Aerodynamica Sinica,2011,29(4):421-426(in Chinese). [11] 陈坚强,陈琦,袁先旭,等.方形截面飞行器上仰机动对滚转特性影响的数值模拟[J].航空学报,2016,37(8):2565-2573. CHEN J Q,CHEN Q,YUAN X X,et al.Numerical simulation of rolling characteristics in nose-up process of square cross section vehicle[J].Acta Aeronautica et Astronautica Sinica,2016,37(8):2565-2573(in Chinese). [12] 陈琦,陈坚强,袁先旭,等.方形截面弹俯仰振荡对滚转特性的影响[J].力学学报,2016,48(6):1281-1289.CHEN Q,CHEN J Q,YUAN X X,et al.Numerical study of the effect of forced pitching oscillation on rolling characteristics of vehicle[J].Chinese Journal of Theoretical and Applied Mechanics,2016,48(6):1281-1289(in Chinese). [13] TARPLEY C,LEWIS M.Stability derivatives for engine integrated waveriders with viscous and pitch effects[C]//32nd AIAA Aerospace Sciences Meeting and Exhibit.Reston:AIAA,1994:1-13. [14] TARPLEY C,LEWIS M J.Stability derivatives for a hypersonic caret-wing waverider[J].Journal of Aircraft,1995,32(4):795-803. [15] RUDD L,PINES D,TARPLEY C.Dynamic stability of mission-oriented hypersonic waveriders[C]//37th AIAA Aerospace Sciences Meeting and Exhibit.Reston:AIAA,1999:1-12. [16] BAUMANN E,BAHM C,STROVERS B,et al.The X-43A six degree of freedom Monte Carlo analysis[C]//46th AIAA Aerospace Sciences Meeting and Exhibit.Reston:AIAA,2008:1-38. [17] KENNELL C,NEELY A,O'BYRNE S,et al.Measurement of vehicle stability coefficients in hypersonic wind tunnels[C]//20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.Reston:AIAA,2015:1-12. [18] YE Y D,ZHAO Z L,TIAN H,et al.The stability analysis of rolling motion of hypersonic vehicles and its validations[J].Science China Physics,Mechanics & Astronomy,2014,57(12):2194-2204. [19] YE Y D,TIAN H,ZHANG X F.The stability of rolling motion of hypersonic vehicles with slender configuration under pitching maneuvering[J].Science China Physics,Mechanics & Astronomy,2015,58(6):1-9. [20] 李乾,赵忠良,叶友达,等.一种临近空间飞行器静/动态气动特性研究[J].空气动力学学报,2017,35(4):504-509.LI Q,ZHAO Z L,YE Y D,et al.Numerical and experimental investigation on aerodynamic characteristics for one typical near space vehicle[J].Acta Aerodynamica Sinica,2017,35(4):504-509(in Chinese). [21] 李乾,赵忠良,王晓冰,等.一种近空间高超声速飞行器滚转稳定性研究[J].航空学报,2018,39(3):1-8.LI Q,ZHAO Z L,WANG X B,et al.Rolling stability research of a near space hypersonic vehicle[J].Acta Aeronautica et Astronautica Sinica,2018,39(3):1-8(in Chinese). [22] 何垒,姚跃民,檀望春,等.高超声速飞行器偏离稳定判据研究[J].弹箭与制导学报,2018,38(4):69-72.HE L,YAO Y M,TAN W C,at al.The research on departure stability criteria for hypersonic vehicle[J].Journal of Projectiles,Rockets,Missiles and Guidance,2018,38(4):69-72(in Chinese). [23] 刘绪.高超声速内外流一体化飞行器动态特性研究[D].长沙:国防科学技术大学,2011:71-78.LIU X.Investigation of dynamic characteristics of hypersonic airframe/propulsion integrative vehicle[D].Changsha:National University of Defense Technology,2011:71-78(in Chinese). [24] 刘绪,刘伟,周云龙,等.吸气式内外流一体化飞行器动导数数值模拟[J].空气动力学学报,2015,33(2):147-155.LIU X,LIU W,ZHOU Y L,et al.Numerical simulation of dynamic derivatives for air-breathing hypersonic vehicle[J].Acta Aerodynamica Sinica,2015,33(2):147-155(in Chinese). [25] 陈琦,谢昱飞,袁先旭,等.内外流一体化飞行器动导数数值预测[J].计算物理,2018,35(5):563-570.CHEN Q,XIE Y F,YUAN X X,at al.Numerical investigation of dynamic derivative forairframe/propulsion integrative vehicles[J].Chinese Journal of Computational Physics,2018,35(5):563-570(in Chinese). [26] 赵忠良,杨晓娟,蒋卫民,等.高超声速飞行器通流模拟方法与风洞验证技术[J].航空学报,2014,35(11):2932-2938. ZHAO Z L,YANG X J,JIANG W M,et al.Through-flow simulation method and wind tunnel validation technique for hypersonic vehicle[J].Acta Aeronautica et Astronautica Sinica,2014,35(11):2932-2938(in Chinese). [27] CHEN J Z,ZHAO Z L,WANG X B,et al.Research on dynamic derivatives test technique for integrative hypersonic vehicle with internal and external flow in wind tunnel[C]//21st AIAA International Space Planes and Hypersonics Technologies Conference.Reston:AIAA,2017:1-7. [28] 姚源,陈萱.美国发SR-72高超声速飞机概念[J].中国航天,2013(12):39-41.YAO Y,CHEN X.America released the SR-72 hypersonic aircraft concept[J].Aerospace China,2013(12):39-41(in Chinese). [29] 丛戎飞,叶友达,赵忠良.吸气式高超声速飞行器俯仰/滚转耦合运动特性[J].航空学报,2020,41(4):123588.CONG R F,YE Y D,ZHAO Z L.Characteristics of air-breathing hypersonic vehicle in force-pitch and free-roll coupling motion[J].Acta Aeronautica et Astronautica Sinica,2020,41(4):123588(in Chinese). [30] 达兴亚,陶洋,赵忠良.基于预估校正和嵌套网格的虚拟飞行数值模拟[J].航空学报,2012,33(6):977-983.DA X Y,TAO Y,ZHAO Z L.Numerical simulation of virtual flight based on prediction correction coupling method and chimera grid[J].Acta Aeronautica et Astronautica Sinica,2012,33(6):977-983(in Chinese). [31] 蒋增辉,宋威,陈农.非旋转钝锥高超声速双平面拍摄风洞自由飞试验[J].力学学报,2015,47(3):406-413.JIANG Z H,SONG W,CHEN N.Hypersonic wind tunnel free-flight test with biplanar optical system on the non-spinning blunt cone[J].Chinese Journal of Theoretical and Applied Mechanics,2015,47(3):406-413(in Chinese). [32] 宋威,赵小见,鲁伟,等.高超声速边界层转捩对旋转钝锥自由飞运动的影响[J].航空学报,2017,38(11):121295.SONG W,ZHAO X J,LU W,et al.Effect of boundary layer transition on free flight motion of hypersonic spinning blunt cone[J].Acta Aeronautica et Astronautica Sinica,2017,38(11):121295(in Chinese). [33] 方振平,陈万春,张曙光.航空飞行器飞行动力学[M].北京:北京航空航天大学出版社,2005:16-32.FANG Z P,CHEN W C,ZHANG S G.Aircraft flight dynamics[M].Beijing:Beihang University Press,2005:16-32(in Chinese). [34] 陶明德.有阻尼Mathieu方程的渐近解[J].应用数学和力学,1992,13(2):187-191.TAO M D.Asymptotic solutions of mathieu equation with damping[J].Applied Mathematics and Mechanics,1992,13(2):187-191(in Chinese). [35] 戎海武,王向东,徐伟,等.Mathieu方程的周期解与稳定性[J].佛山科学技术学院学报(自然科学版),2002,20(3):1-4.RONG H W,WANG X D,XU W,et al.Periodic solution and transition curve of Mathieu equation[J].Journal of Foshan University(Natural Science Edition),2002,20(3):1-4(in Chinese). |