About | Contact Us | Register | Login
ProceedingsSeriesJournalsSearchEAI
sumare 25(1):

Research Article

Aerodynamic Performance Analysis of E387 and S1010 Turbine Blade Profile

Download150 downloads
Cite
BibTeX Plain Text
  • @ARTICLE{10.4108/eetsmre.8435,
        author={Dinh Quy Vu and Van Y Nguyen and Thi Tuyet Nhung Le},
        title={Aerodynamic Performance Analysis of E387 and S1010 Turbine Blade Profile},
        journal={Sustainable Manufacturing and Renewable Energy},
        volume={2},
        number={1},
        publisher={EAI},
        journal_a={SUMARE},
        year={2025},
        month={4},
        keywords={Low Reynolds number, lift to drag ratio, airfoil, turbine blade, aerodynamics},
        doi={10.4108/eetsmre.8435}
    }
    
  • Dinh Quy Vu
    Van Y Nguyen
    Thi Tuyet Nhung Le
    Year: 2025
    Aerodynamic Performance Analysis of E387 and S1010 Turbine Blade Profile
    SUMARE
    EAI
    DOI: 10.4108/eetsmre.8435
Dinh Quy Vu1, Van Y Nguyen1, Thi Tuyet Nhung Le1,*
  • 1: Hanoi University of Science and Technology
*Contact email: nhung.lethituyet@hust.edu.vn

Abstract

This paper investigates the changes in lift and drag coefficients, as well as the lift-to-drag ratio, of two airfoils designed for small wind turbines operating at low Reynolds numbers. The results include 2D simulations performed using the commercial software ANSYS Fluent 2019. The two selected airfoils, EPU-E387 and EPU-S1010, are newly developed and have not yet been studied for their aerodynamic performance. The research method involves varying the angle of attack to determine the optimal angle and identify which airfoil offers greater stability. The Reynolds numbers applied in the 2D simulations include 50,000, 60,000, 90,000, and 120,000. The simulation results indicate that the EPU-E387 airfoil achieves the highest lift-to-drag coefficient at the optimal angle of attack, which is 13.13% greater than that of the EPU-S1010 airfoil at Reynolds number 120,000. Additionally, the EPU-E387 airfoil demonstrates greater stability compared to the EPU-S1010 at higher angles of attack.

Keywords
Low Reynolds number, lift to drag ratio, airfoil, turbine blade, aerodynamics
Received
2025-04-11
Accepted
2025-04-11
Published
2025-04-11
Publisher
EAI
http://dx.doi.org/10.4108/eetsmre.8435

Copyright © 2025 D. Q. Quy et al., licensed to EAI. This is an open access article distributed under the terms of the CC BY-NC-SA 4.0, which permits copying, redistributing, remixing, transformation, and building upon the material in any medium so long as the original work is properly cited.

EBSCOProQuestDBLPDOAJPortico
EAI Logo

About EAI

  • Who We Are
  • Leadership
  • Research Areas
  • Partners
  • Media Center

Community

  • Membership
  • Conference
  • Recognition
  • Sponsor Us

Publish with EAI

  • Publishing
  • Journals
  • Proceedings
  • Books
  • EUDL