Lewis HO, East RA. Measurement of free-flight dynamic stability derivatives of cones in a hypersonic gun tunnel. AIAA No.95-6082, 1995
[2]
马家驩, 唐宗衡, 张小平等. 激波管风洞中锥模型静、动稳定性导数的测量. 力学学报,1980,16(1): 84-89 (Ma Jiahuan, Tang Zongheng, Zhang Xiaoping, et al. The measurements of the static and dynamic stability derivatives of conical models in the shock tunnel. Acta Mechanica Sinica, 1980, 16(1): 84-89 (in Chinese))
[3]
Prislin RH. High-amplitude dynamic-stability characteristics of blunt 10-degree cones. In: Proc. of AIAA 4th Aerospace Sciences Metting, 66-465, 1966
[4]
Nicolaides JD, Ingram CW, Clare TA. An investigation of the non-linear flight dynamics of ordnance weapons. AIAA No. 69-135, 1969
[5]
Ingram CW, Nicolaides JD. Obtaining nonlinear aerodynamic stability coefficients from free-angular motion of rigid bodies. J Spacecraft, 1969, 8(4): 390-395
[6]
Nicolaides JD, Ingram CW, Martin JM. Nonlinear aerodynamic stability characteristics of the 2.75 wrap-around fin configuration. In: Proc. of 8th Navy Symposium on Aeroballistics, 1969, 3: 751-832
[7]
Nicolaides JD, Eikenberry RS, Ingram CW, et al. Flight dynamics of the basic finner in various degrees of freedom. AFATL-TR-68-32, 1968
[8]
许可法, 何龙德, 李明娟等. 大攻角风洞自由飞动导数实验研究. 航空学报, 1993,14(8): B394-B397 (Xu Kefa, He Longde, Li Mingjuan, et al. Experimental investigation of dynamic stability derivatives at high angle of attack in wind tunnel free-flight. Acta Aeronautica et Astronautica Sinica, 1993, 14(8): B394-B397 (in Chinese))
[9]
Wey P, Seiler F, Srulijes J, et al. Determination of aerodynamic coefficients from shock tunnel free flight trajectories. AIAA2012-3321, 2012
[10]
Tanno H, Komuro T, Sato K, et al. Free-flight tests of reentry capsule models in free-piston shock tunnel. AIAA2013-2979, 2013
[11]
Prislin RH, Holway HP. A wind tunnel free flight testing technique for nonplanar motion of spinning models. AIAA66-774
[12]
Jaffe P. Nonplanar tests using the wind-tunnel free-flight technique. J Spacecraft, 1973, 10(7): 435-442
[13]
许可法, 王陵志, 李明娟 等. 旋转导弹风洞六自由度自由飞动导数实验研究. 空气动力学学报, 1993, 11(3): 257-262 (Xu Kefa, Wang Lingzhi, Li Mingjuan, et al. Research on dynamic derivative of Spinning missile by six-degree-of-freedom free-flight test in wind tunnel. Acta Aerodynamica Sinica, 1993, 11(3): 257-262 (in Chinese))
[14]
蒋增辉,陈农. 旋转钝锥双平面拍摄风洞自由飞试验. 力学学报, 2013,45(5): 777-781 (Jiang Zenghui, Chen Nong. Wind tunnel free-flight test with biplanar optical system on the spinning blunt cone. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(5): 777-781 (in Chinese))
[15]
马家驩, 李江, 潘文欣等. 有翼飞行器高超声速动导数的风洞自由飞测量.流体力学实验与测量, 2001, 15(4): 70-76 (Ma Jiahuan, Li Jiang, Pan Wenxin, et al. Hypersonic pitching damp measurements for a winged vehicle by model free flight. Experiments and Measurements in Fluid Mechanics, 2001, 15(4): 70-76 (in Chinese))
[16]
李江, 马家驩, 潘文欣等. 两种有翼飞行器高超声速动态气动特性的对比实验研究. 空气动力学学报, 2001, 19(2): 217-222 (Li Jiang, Ma Jiahuan, Pan Wenxin, et al. Comparative experiments of two kinds of space shuttle like model for hypersonic pitching damp by model free flight technology. Acta Aerodynamica Sinica, 2001, 19(2): 217-222 (in Chinese))
[17]
韩子鹏. 弹箭外弹道学. 北京:北京理工大学出版社, 2008: 302-307 (Han Zipeng. Exterior Ballistics of Projectiles and Rockets. Beijing: Beijing Institute of Technology Press, 2008: 302-307 (in Chinese))
[18]
李臣明, 刘怡昕. 非对称赤道阻尼力矩对远程火箭弹道的影响. 弹道学报, 2009, 21(2): 36-39 (Li Chenming, Liu Yixin. Influence of unsymmetrical equatorial damp moment on long-range rockets trajectory. Journal of Ballistics, 2009, 21(2): 36-39 (in Chinese))
[19]
Eikenbery RS. Analysis of the angular motion of missiles. SC-CR-70-6051,1970
[20]
李周复. 风洞特种试验技术. 北京:航空工业出版社, 2010: 328-368 (Li Zhoufu. Wind Tunnel Special Tests Technique. Beijing: Aviation Industry Press, 2010: 328-368 (in Chinese))
[21]
李臣明, 刘怡昕. 大长径比远程弹箭的极限平面摆动及其抑制. 系统仿真学报, 2009, 21(23): 7390-7396 (Li Chenming, Liu Yixin. Limit plane swing motion and its restraining measure of un-rotary long-range missile with large ratio of length to diameter. Journal of System Simulation, 2009, 21(23): 7390-7396 (in Chinese))
[22]
邓超. 弹箭非线性角运动规律研究. [硕士论文]. 南京:南京理工大学,2013. (Deng Chao. Research about the regular pattern of nonlinear angualar movement of projectile. [Master Thesis]. Nanjing: Nanjing University of Science & Technology, 2013 (in Chinese))
