[1] 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, 2011:1-3. LIU X. Investigation of dynamic characteristics of hypersonic airframe/propulsion integrative vehicle[D]. Changsha:National University of Defense Technology, 2011:1-3(in Chinese).
[2] WEINACHT P. Navier-Stokes predictions of pitch damping for a family of flared projectiles:AIAA-1991-3339[R]. Reston:AIAA, 1991.
[3] QIN N, LUDLOW D K, SHAW S T, et al. Calculation of pitch damping coefficients for projectiles:AIAA-1997-0405[R]. Reston:AIAA, 1997.
[4] 刘伟, 张鲁民. 钝体俯仰阻尼导数数值计算[J]. 空气动力学学报, 1997, 15(4):427-435. LIU W, ZHANG L M. Numerical calculation of damping in pitch derivatives of blunt cone[J]. Acta Aerodynamics Sinica, 1997, 15(4):427-435(in Chinese).
[5] 刘伟, 牟斌. 高超声速滚转阻尼导数数值模拟[J]. 飞行力学, 2000, 18(2):27-29. LIU W, MOU B. Numerical simulation of damping-in-roll derivatives of blunt cone for hypersonic flow[J]. Flight Dynamics, 2000, 18(2):27-29(in Chinese).
[6] 刘伟, 刘君, 柳军. 平衡气体效应对飞行器动态特性的影响研究[J]. 飞行力学, 2004, 22(4):65-68. LIU W, LIU J, LIU J. Investigation of equilibrium gas effect on dynamic characteristic of aerocraft[J]. Flight Dynamics, 2004, 22(4):65-68(in Chinese).
[7] 袁先旭, 张涵信, 谢昱飞. 基于CFD方法的俯仰静、动导数数值计算[J]. 空气动力学学报, 2005, 23(4):458-463. YUAN X X, ZHANG H X, XIE Y F. The pitching static/dynamic derivatives computation based on CFD methods[J]. Acta Aerodynamics Sinica, 2005, 23(4):458-463(in Chinese).
[8] 袁先旭, 陈坚强, 王文正. 平头增阻再入体俯仰动态特性计算与流动机理分析[J]. 空气动力学学报, 2007, 25(3):300-305. YUAN X X, CHEN J Q, WANG W Z. Pitching dynamic stability computation for plane nose reentry vehicle and flow mechanism analysis[J]. Acta Aerodynamics Sinica, 2007, 25(3):300-305(in Chinese).
[9] 袁先旭, 张涵信, 谢昱飞. 飞船返回舱再入俯仰动稳定吸引子数值仿真[J]. 空气动力学学报, 2007, 25(4):431-436. YUAN X X, ZHANG H X, XIE Y F. Numerical simulation for dynamic stability in pitching of unfinned reentry capsule and bifurcation with mach number prediction[J]. Acta Aerodynamics Sinica, 2007, 25(4):431-436(in Chinese).
[10] BRYAN G, WILLIAMS W. The longitudinal stability of aerial gliders[J]. Proceedings of the Royal Society of London, 1904, 73(488-496):100-116.
[11] TOBAK M, SCHIFF L B. On the formulation of the aerodynamic characteristics in aircraft dynamics:NASA technical report, N76-15082/OSL[R]. Washington, D.C.:NASA, 1976.
[12] ETKIN B, TEICHMANN T. Dynamics of flight:Stability and control[J]. Journal of Guidance Control & Dynamics, 2009, 20(4):839-840.
[13] 任玉新, 刘秋生. 飞行器动态稳定性参数的数值计算方法[J]. 空气动力学学报, 1996, 14(2):117-126. REN Y X, LIU Q S. A numerical method for evaluating aerodynamic stability parameters of vehicles[J]. Acta Aerodynamica Sinica, 1996, 14(2):117-126(in Chinese).
[14] 袁先旭. 非定常流动数值模拟及飞行器动态特性分析研究[D]. 绵阳:中国空气动力研究与发展中心, 2002:111-115. YUAN X X. Numerical simulation for unsteady flows and research on dynamic characteristics of vehicle[D]. Mianyang:China Aerodynamics Research and Development Center, 2002:111-115(in Chinese).
[15] 陈坚强, 陈琦, 袁先旭, 等. 舵面操纵动态响应的数值模拟研究[J]. 力学学报, 2013, 45(2):302-306. CHEN J Q, CHEN Q, YUAN X X, et al. Numerical simulation study on dynamics response under rudder control[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(2):302-306(in Chinese).
[16] 陈琦, 陈坚强, 袁先旭, 等. 谐波平衡法在动导数快速预测中的应用研究[J]. 力学学报, 2014, 46(2):183-190. CHEN Q, CHEN J Q, YUAN X X, et al. Application of a harmonic balance method in rapid predictions of dynamic stability derivatives[J]. Chinese Journal of Theoretical and Applied Mechanics, 2014, 46(2):183-190(in Chinese).
[17] 杨小权, 程苏堃, 杨爱明, 等. 基于时间谱方法的振荡翼型和机翼非定常黏性绕流数值模拟[J]. 航空学报, 2013, 34(4):787-797. YANG X Q, CHENG S K, YANG A M, et al. Time spectral method for numerical simulation of unsteady viscous flow over oscillating airfoil and wing[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(4):787-797(in Chinese).
[18] 刘伟, 杨小亮, 赵云飞. 高超声速飞行器加速度导数数值模拟[J]. 空气动力学学报, 2010, 28(4):426-429. LIU W, YANG X L, ZHAO Y F. Numerical simulation of acceleration derivative of hypersonic aircraft[J]. Acta Aerodynamics Sinica, 2010, 28(4):426-429(in Chinese).
[19] 杨云军, 崔尔杰, 周伟江. 细长三角翼滚转/侧滑耦合运动的数值研究[J]. 航空学报, 2007, 28(1):14-19. YANG Y J, CUI E J, ZHOU W J. Numerical research on roll and sideslip coupling motions about a slender delta-wing[J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(1):14-19(in Chinese).
[20] 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.
[21] 孙涛, 高正红, 黄江涛. 基于CFD的动导数计算与减缩频率影响分析[J]. 飞行力学, 2011, 29(4):15-18. SUN T, GAO Z H, HUANG J T. Identify of aircraft dynamic derivatives based on CFD technology and analysis of reduce frequency[J]. Flight Dynamics, 2011, 29(4):15-18(in Chinese).
[22] COULTER S M, MARQUART E J. Cross and cross-coupling derivative measurements on the standard dynamics model at AEDC:AIAA-1982-0596[R]. Reston:AIAA, 1982.
[23] BUTLER R W. Aircraft motion sensitivity to cross and cross-coupling damping derivatives:NASA technical report, AD-A032654/6SL[R]. Washington, D.C.:NASA, 1977.
[24] BUTLER R W, LANGHAM T F. Sensitivity of aircraft spinning motion to dynamic cross-coupling and acceleration derivatives:NASA technical report, AD-A060516/2SL[R]. Washington, D.C.:NASA, 1979.
[25] LANGHAM T F. Aircraft motion sensitivity to dynamic stability derivatives:AIAA-1979-1621[R]. Reston:AIAA, 1979.
[26] 何植岱. 飞机大迎角稳定性对于交叉导数和加速度导数的灵敏度分析[J]. 空气动力学学报, 1987, 5(4):334-344. HE Z D. Sensitivity of aircraft stability to cross-coupling derivatives and angular acceleration derivatives at high angles of attack[J]. Acta Aerodynamics Sinica, 1987, 5(4):334-344(in Chinese). |