Kun Du

Employment

• Northwestern Polytechnical University Associate Professor
  2019 - Present

Education

• Instituteo f Turbomachinery PhD
  2012 - 2018
• Lund University

Projects & Funding

Projects & funding information is unavailable.

Publications (27)

• Effects of cone angle formed by single-side and double-side laser machining on the aerothermal performance for a plate with multi-rows cooling holes
  Aerospace Science and Technology 2026 DOI: 10.1016/j.ast.2026.112254
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• Effects of Reynolds number and turbulence intensity on endwall film cooling performance considering the variation of the upstream slot
  Thermal Science and Engineering Progress 2026 DOI: 10.1016/j.tsep.2026.104593
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• Influence of pore morphology on thermo-mechanical response of ceramic matrix composite plates
  Aerospace Science and Technology 2026 DOI: 10.1016/j.ast.2026.113143
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• Improved prediction of film cooling effectiveness for flat-surface film holes in gas turbine endwalls and blades by considering turbulent Schmidt number modeling
  Applied Thermal Engineering 2025 DOI: 10.1016/j.applthermaleng.2025.127881
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• Experimental and computational investigation of the regional endwall cooling performance considering influences of film holes layouts and purge slot shape
  Thermal Science and Engineering Progress 2025 DOI: 10.1016/j.tsep.2025.103333
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• Influence of hole blockage caused by thermal barrier coatings on the turbine vane endwall film cooling performance
  International Journal of Thermal Sciences 2025 DOI: 10.1016/j.ijthermalsci.2024.109491
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• Numerical and experimental investigation of film cooling effectiveness distribution predictions that considers the effects of the turbulent Schmidt number
  International Journal of Heat and Mass Transfer 2025 DOI: 10.1016/j.ijheatmasstransfer.2024.126294
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• Experimental and numerical investigations of cooling characteristics on endwall partitioned film cooling with shaped holes
  International Journal of Thermal Sciences 2024 DOI: 10.1016/j.ijthermalsci.2024.109337
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• Modeling and Performance Analysis of Variable Cycle Engine with Ceramic Matrix Composite Turbine Blades
  Aerospace 2024 DOI: 10.3390/aerospace11110886
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• Effect of non-axisymmetric endwall contouring and swirling inlet flow on film cooling performance of turbine endwall
  International Journal of Heat and Mass Transfer 2024 DOI: 10.1016/j.ijheatmasstransfer.2024.125702
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