Michał Przepiórski

Mr. Michał Przepiórski

orcid

Research Focus & Metrics

Academic Career Length

2Years (2025-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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2 July 2026 in Energies
Verified
Journal Article
Open access
PDF file
PLPaweł Ligęza
Paweł Ligęza
MPMichał Przepiórski
Michał Przepiórski
HJHubert Jabłoński
Hubert Jabłoński
The paper presents the concept of a turbine-based energy harvester designed to recover kinetic energy from airflow generated by a moving vehicle and integrated with a roadside acoustic barrier. The proposed solutions employ a vertical-axis aerodynamic turbine positioned within a cavity in the barrier and various airflow guiding structures intended to enhance the efficiency of energy transfer from turbulent airflow to the turbine rotor. To evaluate the effectiveness of the proposed concepts, two-dimensional CFD simulations were conducted in the ANSYS Fluent environment using the k–ε turbulence model. Three airflow deflector geometries and one reference configuration without a deflector were analyzed. The performance of each configuration was assessed based on the maximum instantaneous power and the average power generated by the turbine during a single vehicle pass-by event. The results demonstrated a significant influence of the airflow guide geometry on system performance. The most effective configuration achieved an average power output of approximately 7 W during a single vehicle pass-by event, whereas the configuration without an airflow guide exhibited significantly lower energy recovery efficiency. The obtained findings confirm the potential of the analyzed technology as a power source for autonomous low-power roadside infrastructure systems.

1 January 2025
Verified
Book Chapter
Closed access
AGAkademia Górniczo-Hutnicza
Akademia Górniczo-Hutnicza
MPMichał Przepiórski
Michał Przepiórski
KSKonrad Staruch
Konrad Staruch
This paper describes the design and implementation of a closed-circuit wind tunnel for PIV testing. The tunnel has a working cross-section of 0.8 m x 0.8 m and allows for flow velocities of up to 10 m/s. The entire system was designed in a CAD environment, and key components were designed using the CFD method.