Citation: | LÜ Jinzhou, ZHANG Xiaoqing, ZHAO Xiaonan, CHEN Guangxiong, WU Yingchuan. Structural Dynamic Characteristics of Force-Measurement System for Impulse Wind Tunnel[J]. Journal of Southwest Jiaotong University, 2019, 54(6): 1305-1313. doi: 10.3969/j.issn.0258-2724.20170737 |
STALKER R J. A study of the free-piston shock tunnel[J]. AIAA Journal, 1967, 5(12): 2160-2165.
|
PATE S R, SILM L G, STALLINGS D W, et al. Development of an MHD-augmented,high enthalpy,shock tunnel facility[J]. AIAA Journal, 1974, 12(3): 289-297. doi: 10.2514/3.49223
|
OLIVIER H, GROENIG H, BOZEC A L. Hypersonic model testing in a shock tunnel[J]. AIAA Journal, 1995, 33(2): 262-265. doi: 10.2514/3.12429
|
ROBINSON M J, MEE D J, TSAI C Y, et al. Three-component force measurements on a large scramjet in a shock tunnel[J]. Journal of Spacecraft & Rockets, 2004, 41(3): 416-425.
|
SCHULTZ I A, GOLDENSTEIN C S, STRAND C L, et al. Hypersonic scramjet testing via diode laser absorption in a reflected shock tunnel[J]. Journal of Propulsion & Power, 2014, 30(6): 1586-1594.
|
TANNO H, KOMURO T, SATO K, et al. Aerodynamic force measurement technique with accelerometers in the impulsive facility HIEST[M]//Shock Waves. Berlin: Springer, 2009: 471-476.
|
TANNO H, KOMURO T, TAKAHASHI M, et al. Unsteady force measurement technique in shock tubes[J]. Review of Sci-entific Instruments, 2004, 75(2): 532-536. doi: 10.1063/1.1641156
|
SINGH P, MENEZES V, IRIMPAN K J, et al. Impulse force bal-ance for ultrashort duration hypersonic test facili-ties[DB/OL]. (2015-5-24)[2017-08-18]. https://www.hindawi.com/journals/sv/2015/803253/.
|
SINGH P, TRIVEDI S, MENEZES V, et al. Dynamic calibration and validation of an accelerometer force balance for hypersonic lifting models[J]. The Scientific World Journal, 2014, 2014(6): 813759.
|
TRIVEDI S, MENEZES V. Measurement of yaw,pitch and ide-force on a lifting model in a hypersonic shock tunnel[J]. Measurement, 2012, 45(7): 1755-1764. doi: 10.1016/j.measurement.2012.04.008
|
SATHEESH K, JAGADEESH G. Analysis of an internally mount-able accelerometer balance system for use with non-isotropic models in shock tunnels[J]. Measurement, 2009, 42(6): 856-862. doi: 10.1016/j.measurement.2009.01.010
|
SARAVANAN S, JAGADEESH G, REDDY K P J. Aerodynamic force measurement using 3-component accelerometer force balance system in a hypersonic shock tunnel[J]. Shock Waves, 2009, 18(6): 425-435. doi: 10.1007/s00193-008-0172-8
|
SMITH A L, MEE D J, DANIEL W J T, et al. Design,modelling and analysis of a six component force balance for hypervelocity wind tunnel testing[J]. Computers & Structures, 2001, 79(11): 1077-1088.
|
LAURENCE S J, HORNUNG H G. Image-based force and mo-ment measurement in hypersonic facilities[J]. Experiments in Fluids, 2009, 46(2): 343-353. doi: 10.1007/s00348-008-0565-6
|
LAURENCE S J, KARL S. An improved visualization-based force-measurement technique for short-duration hypersonic facilities[J]. Experiments in Fluids, 2010, 48(6): 949-965. doi: 10.1007/s00348-009-0780-9
|
刘洪山,徐翔,姜华. 应力波天平在国内激波风洞上的应用[J]. 实验流体力学,2006,20(1): 36-39. doi: 10.3969/j.issn.1672-9897.2006.01.009
LIU Hongshan, XU Xiang, JIANG Hua, et al. The application of the stress wave force balance in shock tunnel[J]. Journal of Experiments in Fluid Mechanics, 2006, 20(1): 36-39. doi: 10.3969/j.issn.1672-9897.2006.01.009
|
WANG Yunpeng, LIU Y, LUO C, et al. Force measurement using strain-gauge balance in a shock tunnel with long test duration[J]. Review of Scientific Instruments, 2016, 87(5): 1068.
|
WANG Y, LIU Y, JIANG Z. Design of a pulse-type strain gauge balance for a long-test-duration hypersonic shock tunnel[J]. Shock Waves, 2016, 26(6): 1-10.
|
贺伟,童泽润,李宏斌. 单模块超燃发动机推力测量天平研制[J]. 航空动力学报,2006,20(1): 36-39. doi: 10.3969/j.issn.1000-8055.2006.01.007
HE Wei, TONG Zerun, LI Hongbin. Investigation of thrust balance for the single module scramjet[J]. Journal of Aerospace Power, 2006, 20(1): 36-39. doi: 10.3969/j.issn.1000-8055.2006.01.007
|
王锋,贺伟,毛鹏飞,等. 脉冲风洞测力系统建模与载荷辨识方法研究[J]. 振动与冲击,2015,34(1): 94-103.
WANG Feng, HE Wei, MAO Pengfei, et al. Dynamic modeling of testing system in impulse facilities and load identification method[J]. Journal of Vibration and Shock, 2015, 34(1): 94-103.
|
程忠宇,陈宏,张琦. 多加速度计振动分离惯性补偿测力技术[J]. 流体力学实验与测量,1999,13(4): 57-61. doi: 10.3969/j.issn.1672-9897.1999.04.012
CHENG Zhongyu, CHEN Hong, ZHANG Qi. Inertia compensation technology based on multi-accelerometer vibration separating[J]. Experiments and Measurements in Fluid Mechanics, 1999, 13(4): 57-61. doi: 10.3969/j.issn.1672-9897.1999.04.012
|