SciELO - Scientific Electronic Library Online

 
 issue104Analytical performance evaluation of GFDM in underwater acoustic communication systemsSustainability performance assessment of the transport sector in European countries author indexsubject indexarticles search
Home Pagealphabetic serial listing  

Services on Demand

Journal

Article

Indicators

Related links

  • On index processCited by Google
  • Have no similar articlesSimilars in SciELO
  • On index processSimilars in Google

Share


Revista Facultad de Ingeniería Universidad de Antioquia

Print version ISSN 0120-6230On-line version ISSN 2422-2844

Abstract

BURBANO-HERNANDEZ, Andres; HINCAPIE, Diego; GRACIANO-URIBE, Jonathan  and  TORRES-LOPEZ, Edwar. Effect of the opening and location ratio on the performance of an H-Darrieus VAWT. Rev.fac.ing.univ. Antioquia [online]. 2022, n.104, pp.33-41.  Epub Mar 24, 2023. ISSN 0120-6230.  https://doi.org/10.17533/udea.redin.20210737.

Vertical axis wind turbines such as Darrieus turbines are a very interesting category of low wind speed domestic wind turbines. Further research work is needed to enhance their efficiency to fulfill the higher demand in small applications for power generation. The main objective of this work is to find a Darrieus turbine design to boost the starting capacity of the turbine through an opening located at the lower surface of the airfoil. We carried out a thorough CFD (Computational Fluid Dynamics) investigation to determine the impact of the opening position on the Darrieus rotor's output. This new type of airfoil uses a standard NACA 0015 profile and a profile with an opening on the lower surface of the profile. Different sizes of the opening in a symmetrical profile are evaluated through the CFD method to predict the C p and C T of this H-Darrieus turbine design. Five sections were designed to describe the research of this new H-Darrieus rotor. Generally speaking, the results showed that the C p decreases with the opening ratio, the desirable rotors with the lower surface opening ratio are 0.12 to 0.36 considering this with the low C p LP.

Keywords : H-Darrieus; Airfoil; ratio; CFD; NACA; Efficiency.

        · abstract in Spanish     · text in English     · English ( pdf )