主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
水翼型水上飞机偏转机翼布局数值研究
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南京航空航天大学直升机旋翼动力学国家级重点实验室

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V211.51

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Numerical Research on the Layout for Wing-Deflectable Hydrofoil Seaplane
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Affiliation:

1.National Key Laboratory of Rotorcraft Aeromechanics,Nanjing University of Aeronautics Astronautics,Nanjing,210016;2.China

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    摘要:

    传统水上飞机水面起飞过程阻力峰值较大,提出一种可偏转机翼水翼型水上飞机,飞机水面滑行时偏转机翼割划水面产生水动升力将飞机抬离水面降低阻力,空中飞行时偏转机翼根据飞行条件可偏转角度。采用空气动力和水动力耦合求解并结合动力学平衡方程方法分析该布局水动特性及空中巡航气动特性,同时计算同尺寸双浮筒型水上飞机水动与气动特性,比较两种构型水动与气动特性。结果表明:水面起飞过程中水翼型水上飞机总阻力峰值约为双浮筒型水上飞机偏转机翼布局的50.7%;飞机空中飞行时,偏转机翼偏转角为0°时气动性能最优且所受阻力低于双浮筒型水上飞机,从而证明水翼型水上飞机偏转机翼布局能够有效提高水上飞机的水动与气动性能。

    Abstract:

    Aiming at the problem of big drag during takeoff for seaplane, a hydrofoil seaplane with deflectable wings is proposed. The hydrodynamic lift generated by deflectable wing cutting the water surface during takeoff is big enough to lift the aircraft off the water surface. The deflectable wing can deflect the angle according to flight conditions during the flight phase. Aerodynamic and hydrodynamic coupling solutions and dynamic equilibrium equations are used to calculate the hydrodynamic performance for hydrofoil seaplane, and the aerodynamic characteristics of air cruise are analyzed. At the same time, the calculation of the same size double-float seaplane is carried out, and the hydrodynamic and aerodynamic characteristics for two configurations were compared. The numerical results show that the peak value of total drag for double-float seaplane is about 1.97 times of that of the deflection wing for hydrofoil seaplane during takeoff. Aerodynamic performance of deflecting wing with 0° deflection angle is optimal and the drag is lower than that of double-float seaplane during flight, which proves that the deflection wing layout of hydrofoil seaplane can effectively improve the hydrodynamic and aerodynamic performance for seaplane.

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引用本文

申遂愿,朱清华,曾嘉楠,朱振华,王坤.水翼型水上飞机偏转机翼布局数值研究[J].航空工程进展,2019,10(6):750-758

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历史
  • 收稿日期:2018-12-24
  • 最后修改日期:2019-03-15
  • 录用日期:2019-03-27
  • 在线发布日期: 2019-12-30
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