AEROSPACE SHANGHAI, Volume. 41, Issue 4, 27(2024)

Study on Attitude-orbit Control Interference Performance of Grid Fin Layout

Xiaolin LI*... Fan YANG, Kai WANG, Wanghao WU and Yinkai MA |Show fewer author(s)
Author Affiliations
  • Shanghai Electromechanical Engineering Institute,Shanghai201109,China
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    Figures & Tables(17)
    Sizes of the standard model (unit:mm)
    Meshes of the grid fin and missile body
    Comparison of the calculated and experimental normal force coefficients
    Structure meshes of the CCF model
    Distribution of the pressure coefficient
    ×-× layout and ×-+ layout
    Nmbering diagram of the jets and grid fins of the ×-× layout and ×-+ layout
    Meshes of the layout with grid fins
    Aerodynamic coefficients of different jet combinations of the ×-× layout
    Aerodynamic coefficients of different jet combinations of the ×-+ layout
    Interference of different layouts under longitudinal jets
    Interference of different layouts under longitudinal jets
    Pressure coefficient distributions with and without jets under the ×-× layout
    Streamlines of the ×-+ layout
    Pressure coefficient contours of the lateral jet field
    Pressure coefficient contours of the longitudinal jet field
    Aerodynamic interference of jets on the components
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    Xiaolin LI, Fan YANG, Kai WANG, Wanghao WU, Yinkai MA. Study on Attitude-orbit Control Interference Performance of Grid Fin Layout[J]. AEROSPACE SHANGHAI, 2024, 41(4): 27

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    Paper Information

    Category: Aerospace Aerodynamics and Test Technology

    Received: Apr. 10, 2024

    Accepted: --

    Published Online: Nov. 18, 2024

    The Author Email:

    DOI:10.19328/j.cnki.2096-8655.2024.04.004

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