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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    References(6)

    [12] M DEBIASI. Forces and moments generated by swept-forward grid fins and planar fins. Journal of Aircraft, 57, 167-172(2020).

    [13] M DEBIASI, Y ZENG. Forces and moments generated by swept-back grid fins with sharp leading edges. Journal of Aircraft, 53, 1964-1968(2016).

    [14] K YE, Y ZHANG, Z CHEN et al. Numerical investigation of aeroelastic characteristics of grid fin. AIAA Journal, 60, 1-15(2022).

    [15] A C KURIAN, B SANTHOSH, P D SHAJI et al. Structural design,development and qualification tests of grid fin. Current Science, 120, 141(2021).

    [22] W D WASHINGTON, M S MILLER. Grid fins-a new concept for missile stability and control(1993).

    [26] P GNEMMI, H J SCHÄFER. Experimental and numerical investigations of a transverse jet interaction on a missile body(2005).

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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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