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A review on aero-engine inlet-compressor integration and inlet flow distortion in axial compressors

Zhenyu Li1,2, Dakun Sun1, Xu Dong3,4

  • 1School of Energy and Power Engineering, Beihang University, Beijing 100191, China.

Fundamental Research
|December 30, 2025
PubMed

Keywords:
Aero-engine intakeAxial compressorFlow stabilityInlet distortionInlet-engine compatibility

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