Open Access
Issue
JNWPU
Volume 39, Number 4, August 2021
Page(s) 786 - 793
DOI https://doi.org/10.1051/jnwpu/20213940786
Published online 23 September 2021
  1. Liao Daxiong, Chen Jiming, Peng Qiang, et al. Key design techniques of the low noise continuous transonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(4): 74–78 [Article] (in Chinese) [Google Scholar]
  2. Chen Dehua, Yin Luping, Wu Wenhua, et al. The test technique for aircraft with high aspect ratio in the 2.4 meter transonic wind tunnel[J]. Acta Aerodynamica Sinica, 2009, 27(5): 542–546 [Article] (in Chinese) [Google Scholar]
  3. Bope Au, Gernk Li. High speed wind tunnel testing[M]. Deng Zhenying, Li Yanlin, translated. Beijing: Science Press, 1983 (in Chinese) [Google Scholar]
  4. Wu Shenghao, Fei Haitao, Chen Jiming, et al. Application of center-line probe in transonic wind tunnel[J]. Journal of Aerospace Power, 2018, 33(10): 2451–2457 [Article] (in Chinese) [Google Scholar]
  5. Liu Zhengchong, Liao Daxiong, Dong Yixin, et al. Aerodynamic and structural design of high and low speed wind tunnel[M]. Beijing: National Defense Industry Press, 2003: 282–283 (in Chinese) [Google Scholar]
  6. Jackson F M. Calibration of the AEDC-PWT 16-ft transonic tunnel at test section wall porosities of two, four, and six percent[R]. AEDC-TR-76-13, 1976 [Google Scholar]
  7. Reed T D. Calibration of transonic and supersonic wind tunnels[R]. NASA-CR-2920, 1987 [Google Scholar]
  8. Dick R S. The influence of several cable-type supports upon the static pressures along the centerline tube in a transonic wind tunnel[R]. AEDC-TN-54-26, 1955 [Google Scholar]
  9. Jackson F M. Supplemental calibration results for the AEDC propulsion wind tunnel(l6T)[R]. AEDC-TR-70-l63, 1970 [Google Scholar]
  10. Chen Dehua, Wang Weixin, Wang Jinjun, et al. Investigation on flow-field debugging for 2.4 m transonic wind tunnel[J]. Acta Aerodynamica Sinica, 2004, 22(3): 279–282 [Article] (in Chinese) [Google Scholar]
  11. Chen Dehua, Wang Ruibo, Liu Guangyuan, et al. The test and flow field calibration of 2.4 m transonic wind tunnel slotted test section[J]. Journal of Experiments in Fluid Mechanics, 2013, 27(4): 66–70 [Article] (in Chinese) [Google Scholar]
  12. Liu Guangyuan, Wang Ruibo, Guo Qiuting, et al. Wall parameters influence on centerline flow uniformity in 2.4 m transonic wind tunnel[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(9): 2930–2938 [Article] (in Chinese) [Google Scholar]
  13. Li Feng, Gao Cao, Zhang Zhengke, et al. The test of characteristics of flow area and calibration model in NF-6 pressurized continuous transonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2013, 27(1): 61–64 [Article] (in Chinese) [Google Scholar]
  14. Charlie M J. Description and calibration of the langley unitary plan wind tunnel[R]. NASA-TP-1905 [Google Scholar]
  15. Bobbitt C J. National transonic Facility characterization status[R]. AIAA-2000-0293 [Google Scholar]
  16. Kohzai M, Ueno M, Shiohara T, et al. Calibration of the test section mach number in the jaxa 2 m×2 m transonic wind tunnel[R]. AIAA-2008-0848 [Google Scholar]
  17. Xiong Bo, Zhou Enmin, Cheng Song, et al. Research on key technologies of debugging and operating in 0.6 m×0.6 m continuous transonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(4): 81–86 [Article] (in Chinese) [Google Scholar]
  18. Li Zhuangsheng, Yang Pengcheng, Chen Dan, et al. The design of total pressure control strategy for 0.6 m continuous transonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(4): 87–92 [Article] (in Chinese) [Google Scholar]
  19. Pang Yinliang, Song Weidong, Yang Xiaolin, et al. Fluent-based aerodynamic simulation of terminal guided projectile in its initial stage[J]. Ordnance Industry Automation, 2009, 28(2): 13–15 [Article] (in Chinese) [Google Scholar]
  20. Zhang Yancheng. Numerical research of flow fieldof fins rocket[D]. Taiyuan: North University of China, 2011: 11-42 (in Chinese) [Google Scholar]
  21. Chevalier H L. Calibration of the PWT 16-ft transonic circuit with a modified model support system and test section[R]. AEDC-TN-60-164, 1960 [Google Scholar]

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