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Numerical Simulation of Hybrid Laminar Flow Control on the Vertical Tail of a General Aircraft
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Kun Gao1, Meng Wei1, Tiejun Zhang2, Hejun Qin1, Qing Wen1
Aerodynamic Research & Experiment | 2025, 3(5) : 59 - 68
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Aerodynamic Research & Experiment | 2025, 3(5): 59-68
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Numerical Simulation of Hybrid Laminar Flow Control on the Vertical Tail of a General Aircraft
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Kun Gao1, Meng Wei1, Tiejun Zhang2, Hejun Qin1, Qing Wen1
Affiliations
  • 1.AVIC General Huanan Aircraft Industry Co.,Ltd.,Zhuhai 519040,China
  • 2.AVIC Aerodynamics Research Institute, Shenyang 110034, China
Published: 2025-09-10 doi: 10.20118/j.issn2097-258X.2025.05.005
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This paper provides technical support for the engineering application of hybir laminar flow control (HLFC)technology in drag reduction for general aircraft. A numerical investigation of HLFC technology for drag reduction on the vertical tail of the AG300 business aircraft is presented. The simulations are based on the Reynolds-Averaged Navier-Stokes (RANS) equations, employing the k SST turbulence model coupled with the γ-transition model. The transition prediction method was validated using experimental data of the infinite swept NLF(2)-0415 airfoil, demonstrating high accuracy and reliability. This paper evaluates the drag reduction effects of uniform suction, non-uniform suction distributions, and reduced leading-edge sweep angle under suction conditions. The results indicate that HLFC can significantly reduce vertical tail drag, with further drag reduction achieved by decreasing the leading-edge sweep angle.However, to maintain flow stability, the suction intensity must be kept below a critical threshold.

HLFC  /  boundary-layer suction  /  drag reduction  /  transition prediction  /  general aircraft
Kun Gao, Meng Wei, Tiejun Zhang, Hejun Qin, Qing Wen. Numerical Simulation of Hybrid Laminar Flow Control on the Vertical Tail of a General Aircraft[J]. Aerodynamic Research & Experiment, 2025 , 3 (5) : 59 -68 . DOI: 10.20118/j.issn2097-258X.2025.05.005
Year 2025 volume 3 Issue 5
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Article Info
doi: 10.20118/j.issn2097-258X.2025.05.005
  • Receive Date:2025-07-23
  • Online Date:2026-03-27
  • Published:2025-09-10
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  • Received:2025-07-23
  • Revised:2025-09-04
Affiliations
    1.AVIC General Huanan Aircraft Industry Co.,Ltd.,Zhuhai 519040,China
    2.AVIC Aerodynamics Research Institute, Shenyang 110034, China
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表12种不同金属材料的力学参数

Family
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Number of
genus
种数
Number of
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占总种数比例
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种数
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鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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