Volume 33 Issue 6
Dec.  2019
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Bi Lin, Li Zhenqian, Tang Zhigong, et al. Study on the efficiency of a new central-type diffuser for hypersonic low density wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(6): 28-33. doi: 10.11729/syltlx20190063
Citation: Bi Lin, Li Zhenqian, Tang Zhigong, et al. Study on the efficiency of a new central-type diffuser for hypersonic low density wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(6): 28-33. doi: 10.11729/syltlx20190063

Study on the efficiency of a new central-type diffuser for hypersonic low density wind tunnel

doi: 10.11729/syltlx20190063
  • Received Date: 2019-05-13
  • Rev Recd Date: 2019-09-03
  • Publish Date: 2019-12-25
  • The diffuser is one of the key components of the supersonic and hypersonic wind tunnels, which directly affects the efficiency-cost ratio of the wind tunnel operation. However, for the hypersonic low density wind tunnel, the range of operating parameters is large and the test gas density is relatively low, and thus the effects of the conventional diffuser with "contraction section, equi-straight section and expansion section" are not obvious. In this paper, a new central-type diffuser structure is presented, and the efficiency of the central-type diffuser is tested at the Φ300 mm hypersonic low density wind tunnel for M16 small flow rate states and M8 large flow rate states. At the same time, the influence of the test section model on the diffuser's capacity is analyzed. The results show that the central-type diffuser has a wide range of operation parameters and a significant pressure increase efficiency, and can effectively improve the wind tunnel test capability. This study can provide a reference for the design of the hypersonic wind tunnel diffuser.
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  • [1]
    Matsuo K, Miyazato Y, Kim H. Shock train and pseudo-shock phenomena in internal gas flows[J]. Progress in Aerospace Sciences, 1999, 35(1): 33-100. doi: 10.1016/S0376-0421(98)00011-6
    [2]
    童华, 孙启志, 张绍武.高超声速风洞扩压器试验研究与分析[J].实验流体力学, 2014, 28(3): 78-81, 103. http://d.old.wanfangdata.com.cn/Periodical/ltlxsyycl201403011

    Tong H, Sun Q Z, Zhang S W. Investigation and analyse on the diffuser of hypersonic wind tunnel[J]. Jounal of Experiments in Fluid Mechanics, 2014, 28(3): 78-81, 103. http://d.old.wanfangdata.com.cn/Periodical/ltlxsyycl201403011
    [3]
    博普A, 戈因K L.高速风洞试验[M].邓振瀛, 译.北京: 科学出版社, 1980.
    [4]
    Neumann E P, Lustwerk F. Supersonic diffusers for wind tunnls[J]. J Appl Mech, 1949, 16(2): 195-202.
    [5]
    Neumann E P, Lustwerk F. High efficiency supersonic diffusers[J]. J Aeronaut Sci, 1951, 18(6): 369-374. doi: 10.2514/8.1975
    [6]
    李桦, 范晓樯, 丁猛.超声速扩压器中激波串结构的数值模拟[J].国防科技大学学报, 2002, 24: 18-21. http://d.old.wanfangdata.com.cn/Periodical/gfkjdxxb200201005

    Li H, Fan X Q, Ding M. Numerical simulation of the shock train structure in the supersonic diffuser[J]. Journal of National University of Defense Technology, 2002, 24: 18-21. http://d.old.wanfangdata.com.cn/Periodical/gfkjdxxb200201005
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