Aerospace (Apr 2024)

Research on the Flow Mechanism of a High-Loading Biomimetic Low-Pressure Turbine Cascade

  • Hanliu Deng,
  • Zhijun Lei,
  • Xiaoqing Ouyang,
  • Yuxiang He,
  • Hang Yuan,
  • Gang Li,
  • Yanfeng Zhang,
  • Xingen Lu,
  • Gang Xu

DOI
https://doi.org/10.3390/aerospace11040328
Journal volume & issue
Vol. 11, no. 4
p. 328

Abstract

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The biomimetic turbine has an excellent flow drag reduction ability and wide incidence adaptability, so it has the potential to achieve high efficiency within a wide working range of high-performance variable cycle engines. A biomimetic cascade that can broaden the effective working incidence angles was designed based on a high-loading low-pressure turbine cascade, and its flow mechanism and aerodynamic performance were studied using experimental and numerical methods under the incidences angle (i) of 0° to 15° and Reynolds number of 1.0 × 105. A series of counter rotating vortex pairs induced by the biomimetic cascade bring additional dissipation losses, but it accelerates the energy exchange between the boundary layer and mainstream, enhancing the dissipation of the pressure side leg of horseshoe vortex, and thus suppressing the flow separation and passage vortices. The undulating surface of biomimetic cascades can suppress the expansion of secondary flow in a spanwise direction in the end region, especially for large-scale separation under high incidence conditions. When i 5°, the losses of biomimetic cascades are significantly reduced, with a maximum reduction of 70% at i = 15°.

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