Spacecraft Recovery & Remote Sensing, Volume. 45, Issue 4, 18(2024)

Planform Geometry Effect on Aerodynamic Performance of Parafoils

Ziyue CHEN1...2, Bowen QIU1,2, Yanjun LI1,2, and Li YU12,* |Show fewer author(s)
Author Affiliations
  • 1Key Laboratory of Aircraft Environment Control and Life Support, Ministry of Industry and Information Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • 2College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
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    References(11)

    [3] [3] NICOLAIDES J D. Parafoil Wind Tunnel Test[M]. Indiana: University of Notre Dame, 1971: 174182.

    [4] [4] FURFARO J, HAILEY C E, BEHR V, et al. An Experimental Study of Parafoil Sections[C]14th AIAA Aerodynamic Decelerat Systems Technology Conference, June 35, 1997, San Francisco, CA, USA. Reston, VA: AIAA, 1997: 1527. DOI: 10.25146.19971527.

    [5] [5] SEIDEL J, LATSCHA C, VENKATARAMAN G, et al. Rigid Ramair Parachute Experiments with Bleed Air Vents[C]54th AIAA Aerospace Sciences Meeting, January 48, 2016, San Diego, Califnia, USA. Reston, VA: AIAA, 2016: 1562. DOI: 10.25146.20161562.

    [6] [6] ROSS J. Computational Aerodynamics in the Design Analysis of Ramairinflated Wings[C]12th AIAA Aerodynamic Decelerat Systems Technology Conference, May 1013, London, UK. Reston, VA: AIAA, 1993: 126.

    [17] [17] GHEYSHI M, BERGERON K, LOFTHOUSE A J, et al. CFD Calculation of Stability Control Derivatives f Ramair Parachutes[C]AIAA Atmospheric Flight Mechanics Conference, January 48, 2016, San Diego, Califnia, USA. Reston, VA: AIAA, 2016: 1536. DOI: 10.25146.20161536.

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    Ziyue CHEN, Bowen QIU, Yanjun LI, Li YU. Planform Geometry Effect on Aerodynamic Performance of Parafoils[J]. Spacecraft Recovery & Remote Sensing, 2024, 45(4): 18

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    Paper Information

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    Received: Nov. 6, 2023

    Accepted: --

    Published Online: Nov. 1, 2024

    The Author Email: YU Li (yuli_happy@163.com)

    DOI:10.3969/j.issn.1009-8518.2024.04.003

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