Research Article

Performance optimization of low-head vertical axis impulse turbine runners for nozzle angle, nozzle diameter, and nozzle standoff distance using response surface methodology

Volume: 11 Number: 5 October 21, 2025
  • H. N. Lakdawala *
  • V. K. Patel
  • G. P. Bakhru
  • D. N. Modi
EN

Performance optimization of low-head vertical axis impulse turbine runners for nozzle angle, nozzle diameter, and nozzle standoff distance using response surface methodology

Abstract

Pico-scale turbines, such as Turgo and Pelton, are site-specific and show variable performance under various operating and design parameters. Experimental investigation and response surface methodology were combined to optimize the geometrical parameters of Pelton and Turgo turbine runners in the present study. Low-cost, lightweight hybrid runners with 3D-printed buckets and aluminum runner discs with a vertical turbine axis were designed for low-head applications. Multivariate statistical evaluation and response surface methodology were con-ducted using Design Expert 13.0 software, with a central composite design applied to analyze results and optimize parameters through 80 test runs. Quadratic models describing the hydraulic efficiency characteristics of impulse turbine runners were developed via ANOVA. The study examined nozzle diameters (10-14 mm), angles (90°-95°), numbers (1 or 2), and standoff distances (40-60 mm). The optimized condition for the Turgo turbine runner was achieved with a 95° nozzle angle, 14 mm nozzle diameter, and a 40 mm standoff distance. The hydraulic efficiency of 66.19% is found, with significant model parameters having P-values below 0.0001. The findings indicated a maximum efficiency of 66.55% under optimized con-ditions, closely matching the proposed model with an error of 0.54%. Thus, the Turgo turbine is highly efficient and suitable for Pico hydro off-grid applications.

Keywords

References

  1. REFERENCES
  2. [1] Gaiser K, Erickson P, Stroeve P, Delplanque JP. An experimental investigation of design parametcers for pico-hydro Turgo turbines using a response surface methodology. Renew Energy 2016;85:406–418. [CrossRef]
  3. [2] McCarthy MJ, Molloy NA. Review of stability of liquid jets and the influence of nozzle design. Chem Eng J 1974;7:1–20. [CrossRef]
  4. [3] Budiarso, Febriansyah D, Warjito, Adanta D. The effect of wheel and nozzle diameter ratio on the performance of a Turgo turbine with pico scale. Energy Rep 2020;:601–605. [CrossRef]
  5. [4] Alomar OR, Abd HM, Salih MM, Ali FA. Performance analysis of Pelton turbine under different operating conditions: an experimental study. Ain Shams Eng J 2022;13:101684. [CrossRef]
  6. [5] Kholifah N, Setyawan AC, Wijayanto DS, Widiastuti I, Saputro H. Performance of Pelton turbine for hydroelectric generation in varying design parameters. IOP Conf Ser Mater Sci Eng 2018;288:012108. [CrossRef]
  7. [6] Huang F, Mi J, Li D, Wang R. Impinging performance of high-pressure water jets emitting from different nozzle orifice shapes. Geofluids 2020;2020:8831544. [CrossRef]
  8. [7] Gupta V, Prasad V, Khare R. Effect of jet length on the performance of Pelton. Int J Mech Eng Technol 2016;11:11487–11494.

Details

Primary Language

English

Subjects

Biomedical Fluid Mechanics

Journal Section

Research Article

Authors

H. N. Lakdawala * This is me
0000-0003-0056-9005
India

D. N. Modi This is me
Canada

Publication Date

October 21, 2025

Submission Date

August 27, 2024

Acceptance Date

December 25, 2024

Published in Issue

Year 2025 Volume: 11 Number: 5

APA
Lakdawala, H. N., Patel, V. K., Bakhru, G. P., & Modi, D. N. (2025). Performance optimization of low-head vertical axis impulse turbine runners for nozzle angle, nozzle diameter, and nozzle standoff distance using response surface methodology. Journal of Thermal Engineering, 11(5), 1392-1419. https://doi.org/10.14744/thermal.0000983
AMA
1.Lakdawala HN, Patel VK, Bakhru GP, Modi DN. Performance optimization of low-head vertical axis impulse turbine runners for nozzle angle, nozzle diameter, and nozzle standoff distance using response surface methodology. Journal of Thermal Engineering. 2025;11(5):1392-1419. doi:10.14744/thermal.0000983
Chicago
Lakdawala, H. N., V. K. Patel, G. P. Bakhru, and D. N. Modi. 2025. “Performance Optimization of Low-Head Vertical Axis Impulse Turbine Runners for Nozzle Angle, Nozzle Diameter, and Nozzle Standoff Distance Using Response Surface Methodology”. Journal of Thermal Engineering 11 (5): 1392-1419. https://doi.org/10.14744/thermal.0000983.
EndNote
Lakdawala HN, Patel VK, Bakhru GP, Modi DN (October 1, 2025) Performance optimization of low-head vertical axis impulse turbine runners for nozzle angle, nozzle diameter, and nozzle standoff distance using response surface methodology. Journal of Thermal Engineering 11 5 1392–1419.
IEEE
[1]H. N. Lakdawala, V. K. Patel, G. P. Bakhru, and D. N. Modi, “Performance optimization of low-head vertical axis impulse turbine runners for nozzle angle, nozzle diameter, and nozzle standoff distance using response surface methodology”, Journal of Thermal Engineering, vol. 11, no. 5, pp. 1392–1419, Oct. 2025, doi: 10.14744/thermal.0000983.
ISNAD
Lakdawala, H. N. - Patel, V. K. - Bakhru, G. P. - Modi, D. N. “Performance Optimization of Low-Head Vertical Axis Impulse Turbine Runners for Nozzle Angle, Nozzle Diameter, and Nozzle Standoff Distance Using Response Surface Methodology”. Journal of Thermal Engineering 11/5 (October 1, 2025): 1392-1419. https://doi.org/10.14744/thermal.0000983.
JAMA
1.Lakdawala HN, Patel VK, Bakhru GP, Modi DN. Performance optimization of low-head vertical axis impulse turbine runners for nozzle angle, nozzle diameter, and nozzle standoff distance using response surface methodology. Journal of Thermal Engineering. 2025;11:1392–1419.
MLA
Lakdawala, H. N., et al. “Performance Optimization of Low-Head Vertical Axis Impulse Turbine Runners for Nozzle Angle, Nozzle Diameter, and Nozzle Standoff Distance Using Response Surface Methodology”. Journal of Thermal Engineering, vol. 11, no. 5, Oct. 2025, pp. 1392-19, doi:10.14744/thermal.0000983.
Vancouver
1.H. N. Lakdawala, V. K. Patel, G. P. Bakhru, D. N. Modi. Performance optimization of low-head vertical axis impulse turbine runners for nozzle angle, nozzle diameter, and nozzle standoff distance using response surface methodology. Journal of Thermal Engineering. 2025 Oct. 1;11(5):1392-419. doi:10.14744/thermal.0000983

IMPORTANT NOTE: JOURNAL SUBMISSION LINK http://eds.yildiz.edu.tr/journal-of-thermal-engineering