Citation: | Bi Lin, Li Zhenqian, Tang Zhigong, Yuan Xianxu, Chen Hao. 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 |
[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
|
1. |
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