• Infrared and Laser Engineering
  • Vol. 50, Issue 12, 20210182 (2021)
Bing Chen1, Yong Zheng1, Bin Xu1, Houtian Zhang1、2, and Zhanglei Chen1
Author Affiliations
  • 1Information Engineering University, Zhengzhou 450001, China
  • 2Department of Civil Engineering, Luoyang Institute of Science and Technology, Luoyang 471023, China
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    DOI: 10.3788/IRLA20210182 Cite this Article
    Bing Chen, Yong Zheng, Bin Xu, Houtian Zhang, Zhanglei Chen. Beam deflection correction model of wedge-shaped shock waves over hypersonic vehicles[J]. Infrared and Laser Engineering, 2021, 50(12): 20210182 Copy Citation Text show less
    Schematic of wedge-shaped shock waves and beam deflection
    Fig. 1. Schematic of wedge-shaped shock waves and beam deflection
    Load layout[28] and wedge-shaped structure of preliminary vehicle
    Fig. 2. Load layout[28] and wedge-shaped structure of preliminary vehicle
    Deflection angles due to shock wave surfaces at different Mach numbers and angles of incidence
    Fig. 3. Deflection angles due to shock wave surfaces at different Mach numbers and angles of incidence
    CFD results of wedge shock waves at different Mach numbers
    Fig. 4. CFD results of wedge shock waves at different Mach numbers
    Linear relationships between deflection angles and shock wave
    Fig. 5. Linear relationships between deflection angles and shock wave
    Comparison of parameters used in numerical calculation and simplified model
    Fig. 6. Comparison of parameters used in numerical calculation and simplified model
    Ma$\;\beta$/rad ${\rho _2}/{\rho _1}$
    5.00.30391.8491
    5.50.28611.9436
    6.00.27162.0393
    6.50.25962.1359
    7.00.24952.2330
    7.50.24102.3301
    8.00.23362.4270
    Table 1. Shock angles and density ratios at different Mach numbers
    Ma10°20°30°40°50°
    5.00.60401.24681.97782.87454.0825
    5.50.67131.38562.19793.19434.5368
    6.00.73941.52622.42093.51844.9971
    6.50.80811.66802.64593.84545.4615
    7.00.87711.81052.87204.17405.9282
    7.50.94621.95323.09824.50286.3952
    8.01.01522.09553.32394.83086.8611
    Table 2. Deflection angles due to the shock wave surfaces at different Mach numbers and angles of incidence (Unit: ("))
    5.05.56.06.57.07.58.0
    $\Delta \beta $0.03570.08060.03280.04310.00480.06060.0193
    Table 3. Measurement errors of shock wave angles at different Mach numbers (Unit: ("))
    Ma5.06.07.08.0
    0.0000.00000.00000.0000
    0.5°0.18900.22310.25280.2777
    0.37590.44270.50020.5479
    1.5°0.56060.65850.74200.8103
    2.0°0.74280.87030.97791.0648
    2.5°0.92251.07811.20801.3114
    3.0°1.09951.28161.43201.5500
    3.5°1.27371.48081.64991.7808
    4.0°1.44501.67561.86182.0038
    4.5°1.61341.86602.06762.2191
    5.0°1.77882.05192.26732.4269
    Table 4. Process parameters at different Mach numbers ( )
    Bing Chen, Yong Zheng, Bin Xu, Houtian Zhang, Zhanglei Chen. Beam deflection correction model of wedge-shaped shock waves over hypersonic vehicles[J]. Infrared and Laser Engineering, 2021, 50(12): 20210182
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