Dr. DUAN Penghao (段鵬浩)

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Research Output

  1. 2021

  2. Optimization of Turbine Cascade Squealer Tip Cooling Design by Combining Shaping and Flow Injection

    Duan, P. H. & He, L., Nov 2021, In: Journal of Turbomachinery. 143, 11, 111007.

    Research output: Journal Publications and Reviews (RGC: 21, 22, 62) › 21_Publication in refereed journal › peer-review

    Scopus citations: 5
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  3. Study on the mixing characteristics of circular transverse jet in crossflow

    Li, Z., Yuan, Y., Varsegov, V. L., Guo, B., Xiao, B. & Duan, P. H., May 2021, In: Aerospace Science and Technology. 112, 106599.

    Research output: Journal Publications and Reviews (RGC: 21, 22, 62) › 21_Publication in refereed journal › peer-review

    Scopus citations: 4
    Check@CityULib

  4. Study of circular transverse jet - A new method for high-efficiency mixing and combustion in crossflow

    Li, Z., Yuan, Y., Yao, J., Varsegov, V. L., Duan, P. H. & Zhao, L., Apr 2021, In: International Communications in Heat and Mass Transfer. 123, 105207.

    Research output: Journal Publications and Reviews (RGC: 21, 22, 62) › 21_Publication in refereed journal › peer-review

    Scopus citations: 4
    Check@CityULib
  5. 2020

  6. Optimization of turbine squealer tip cooling design by combining shaping and flow injection

    Duan, P. H. & He, L., Sep 2020, Proceedings of the ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers (ASME), Vol. 7C. V07CT13A018. (Proceedings of the ASME Turbo Expo; vol. 7C-2020).

    Research output: Chapters, Conference Papers, Creative and Literary Works (RGC: 12, 32, 41, 45) › 32_Refereed conference paper (with ISBN/ISSN) › peer-review

    Check@CityULib

  7. Application of multiscale methodology for transonic turbine blade tip cooling design

    Duan, P. H. & He, L., Aug 2020, In: Journal of Turbomachinery. 142, 8, 081011.

    Research output: Journal Publications and Reviews (RGC: 21, 22, 62) › 21_Publication in refereed journal › peer-review

    Scopus citations: 6
    Check@CityULib

  8. Numerical aero-thermal study of high-pressure turbine nozzle guide vane: Effects of inflow conditions

    Phan, H. M., Duan, P. H. & Dinh, C. T., Mar 2020, In: Physics of Fluids. 32, 3, 034111.

    Research output: Journal Publications and Reviews (RGC: 21, 22, 62) › 21_Publication in refereed journal › peer-review

    Scopus citations: 8
    Check@CityULib
  9. 2019

  10. Application of multi-scale methodology for transonic turbine blade tip cooling design

    Duan, P. H. & He, L., 2019, Proceedings of the ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers (ASME), Vol. 5B. V05BT22A006. (Proceedings of the ASME Turbo Expo; vol. 5B-2019).

    Research output: Chapters, Conference Papers, Creative and Literary Works (RGC: 12, 32, 41, 45) › 32_Refereed conference paper (with ISBN/ISSN) › peer-review

    Scopus citations: 1
    Check@CityULib
  11. 2018

  12. Loss generation in transonic turbine blading

    Duan, P., Tan, C. S., Scribner, A. & Malandra, A., 1 Apr 2018, In: Journal of Turbomachinery. 140, 4, 041006.

    Research output: Journal Publications and Reviews (RGC: 21, 22, 62) › 21_Publication in refereed journal › peer-review

    Scopus citations: 23
    Check@CityULib
  13. 2017

  14. Loss generation in transonic turbine blading

    Duan, P., Tan, C. S., Scribner, A. & Malandra, A., 2017, Turbomachinery. American Society of Mechanical Engineers (ASME), Vol. 2A-2017. (Proceedings of the ASME Turbo Expo; vol. 2A-2017).

    Research output: Chapters, Conference Papers, Creative and Literary Works (RGC: 12, 32, 41, 45) › 32_Refereed conference paper (with ISBN/ISSN) › peer-review

    Scopus citations: 1
    Check@CityULib