Volume 41 Issue 9
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Yuan Yiqi, Li Yongzhou, Yang Xueliang, et al. Sensitivity analysis of parameters and optimal design of wide range osculating cone waverider[J]. Journal of Aerospace Power, 2026, 41（9）：20240804 doi: 10.13224/j.cnki.jasp.20240804
Citation: Yuan Yiqi, Li Yongzhou, Yang Xueliang, et al. Sensitivity analysis of parameters and optimal design of wide range osculating cone waverider[J]. Journal of Aerospace Power, 2026, 41（9）：20240804 doi: 10.13224/j.cnki.jasp.20240804
shu

Sensitivity analysis of parameters and optimal design of wide range osculating cone waverider

doi: 10.13224/j.cnki.jasp.20240804
  • 1.

    School of Aeronautics and Astronautics，Nanchang Hangkong University，Nanchang 330063，China

  • 2.

    Jiangxi Key Laboratory for Innovative Configuration Aircraft Design，Nanchang Hangkong University，Nanchang 330063，China

  • 3.

    Institute of Mechanics，Chinese Academy of Sciences，Beijing 100190，China

  • 4.

    College of Energy and Power Engineering，Nanjing University of Aeronauties and Astronautics，Nanjing 210016，China

  • Received Date: 2024-11-26
    Available Online: 2026-06-25
    Abstract

  • The osculating cone waverider is studied in order to improve its wide area performance, five parameters, including the leading edge curve function coefficients a and l, shock wave curve function coefficients b and c, and the semi-cone Angle δc of the reference flow field, were selected as the design variables, and the sensitivity analysis of the design parameters was carried out in the range of Ma=4～7. The second generation of non-dominated sorting genetic algorithm is used to optimize the volume ratio, design point Ma6 and non-design point Ma=4 lift-drag ratio as the target variables. The results show a significant nonlinear relationship between the design parameters and the performance parameters, wherein the semi-cone angle of the reference flow field plays a crucial role in determining both the geometric and aerodynamic performance of the waverider. Compared with the reference model, the volume ratio of the optimized waverider is increased by 7.1%. At the design point of Ma=6 and the non-design point of Ma=4, the lift-drag ratio is increased by 3.4% and 10.7%. The optimized waverider over a wide Mach number range shows higher aerodynamic efficiency and lower total pressure loss, with a lift to drag ratio of 4.88 at Ma=7, which can be maintained at 3.90 even after leading edge bluntness. The optimized design significantly enhances the aerodynamic performance of both the design and non-design points of the waverider, and possesses good wide range adaptability.

     

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