Advancements in Tunable Diode Laser Absorption Spectroscopy for Hypersonic Wind Tunnel Testing

被引:0
|
作者
Fang Hongxin [1 ,2 ,3 ]
Zhi Dong [2 ,3 ]
Wu Xuecheng [1 ]
Li Yunfei [2 ,3 ]
Chang Yu [2 ,3 ]
Chen Wei [2 ,3 ]
Kong Rongzong [2 ,3 ]
机构
[1] Zhejiang Univ, Polytech Inst, Hangzhou 310015, Zhejiang, Peoples R China
[2] China Aerodynam Res & Dev Ctr, Hyperveloc Aerodynam Inst, Mianyang 621050, Sichuan, Peoples R China
[3] China Aerodynam Res & Dev Ctr, Lab Aerodynam Multiple Flow Regimes, Mianyang 621050, Sichuan, Peoples R China
关键词
tunable diode laser absorption spectroscopy; hypersonic wind tunnel; flow field diagnosis; temperature; concentration; velocity;
D O I
10.3788/LOP232396
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Hypersonic wind tunnels play a crucial role in aerospace research, and tunable diode laser absorption spectroscopy (TDLAS) serves as an invaluable diagnostic method in this field. TDLAS offers no-contact, highly sensitive, and multiparameter measurement capabilities coupled with a simple structure, cost-effectiveness, and high spatiotemporal resolution. This study introduces the measurement principle and typical optical design of TDLAS, highlighting its widespread use for measuring parameters such as temperature, component concentration, and airflow velocity in extreme environments such as hypersonic wind tunnels. Furthermore, this study provides an overview of recent applications of TDLAS in hypersonic wind tunnel flow field diagnosis globally. Additionally, it summarizes the current development status and challenges of TDLAS in hypersonic wind tunnel flow field diagnosis in China. It concludes with a brief outlook on the prospective development of TDLAS flow field diagnosis technology in hypersonic wind tunnels, offering valuable insights for future advancements and related experiments in this domain.
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收藏
页数:15
相关论文
共 75 条
  • [1] DIODE-LASER ABSORPTION TECHNIQUE FOR SIMULTANEOUS MEASUREMENTS OF MULTIPLE GASDYNAMIC PARAMETERS IN HIGH-SPEED FLOWS CONTAINING WATER-VAPOR
    ARROYO, MP
    LANGLOIS, S
    HANSON, RK
    [J]. APPLIED OPTICS, 1994, 33 (15): : 3296 - 3307
  • [2] Berger K.T., 2015, P 53 AIAA AER SCI M, P1337
  • [3] Boyd ID, 2017, CAMB AERO SER, P1, DOI 10.1017/9781139683494
  • [4] Brandis A, 2010, P 10 AIAA ASME JOINT, P4510
  • [5] Candler G.V., 2015, 53 AIAA AEROSPACE SC, P1, DOI DOI 10.2514/6.2015-1893
  • [6] Chaudhry RossS., 2020, AIAA Scitech 2020 Forum, P2191, DOI [10.2514/6.2020-2191, DOI 10.2514/6.2020-2191]
  • [7] Chen W, 2019, Acta Aeronautica et Astronautica Sinica, V40
  • [8] Dolvin D, 2009, P 16 AIAA DLR DGLR I, P7228
  • [9] Dolvin D., 2008, 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, P1, DOI [10.2514/6.2008-2581, DOI 10.2514/6.2008-2581]
  • [10] Dudas E, 2022, P 9 EUR C AER SCI LI