Flow Control and Beyond Enhancing Performance and Energy Efficiency in Complex Fluid System

A special issue of Actuators (ISSN 2076-0825). This special issue belongs to the section "High Torque/Power Density Actuators".

Deadline for manuscript submissions: 30 September 2025 | Viewed by 2171

Special Issue Editors


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Guest Editor
Department of Electromechanical Engineering, University of Beira Interior, 6200386 Covilhã, Portugal
Interests: renewable energies; plasma actuators; aerodynamics; fluid mechanics; heat transfer
Special Issues, Collections and Topics in MDPI journals

E-Mail Website
Guest Editor
C-MAST, Department of Electromechanical Engineering, Universidade da Beira Interior Portugal, 6200 Covilhã, Portugal
Interests: flow control; atmospheric deicing devices; plasma actuators; energy conversion and energy storage; numerical simulation; enhanced heat transfer; redox flow batteries
Special Issues, Collections and Topics in MDPI journals

Special Issue Information

Dear Colleagues,

This Special Issue aims to attract works related to a diverse range of topics on the implementation of actuators for flow control in complex fluid systems. Fluid systems play a pivotal role in several industrial applications. The ability to manipulate and control flow fields is key for achieving considerable energy efficiency and performance enhancements. Bearing this in mind, this Special Issue intends to disseminate the most recent advances on various themes related to flow control, including the following: advanced flow control techniques; electro-hydro dynamics and magneto-plasma dynamics; novel fluid dynamic modeling approaches; the interplay between flow control techniques; novel actuators for fluid flow manipulation; cutting-edge materials and technologies for active and passive flow control; machine learning methods for smart flow control; and interdisciplinary research at the intersection of fluid dynamics, engineering, and sustainability.

Dr. Frederico Miguel Freire Rodrigues
Dr. M. Abdollahzadeh
Guest Editors

Manuscript Submission Information

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Keywords

  • flow control
  • actuators
  • fluid systems
  • electro-hydro dynamics
  • magneto-plasma dynamics

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Published Papers (4 papers)

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Research

16 pages, 6815 KiB  
Article
Investigating the Power Extraction of Applying Hybrid Pitching Motion on a Wing with Leading and Trailing Flaps
by Suleiman Saleh and Chang-Hyun Sohn
Actuators 2025, 14(2), 62; https://doi.org/10.3390/act14020062 - 27 Jan 2025
Viewed by 433
Abstract
This research utilized a hybrid trajectory on a wing incorporating a dual flap with the goal of enhancing performance. The hybrid profiles initiate with a non-sinusoidal pattern during the interval 0.0 ≤ t/T ≤ 0.25, evolving toward a sinusoidal pattern within the range [...] Read more.
This research utilized a hybrid trajectory on a wing incorporating a dual flap with the goal of enhancing performance. The hybrid profiles initiate with a non-sinusoidal pattern during the interval 0.0 ≤ t/T ≤ 0.25, evolving toward a sinusoidal pattern within the range 0.25 < t/T ≤ 0.5. Similarly, the hybrid motion follows a non-sinusoidal pattern in the range 0.5 < t/T ≤ 0.75, before shifting back to a sinusoidal pattern within the range 0.75 < t/T ≤ 1.0. The effectiveness of using a hybrid trajectory on a wing with leading and trailing flaps in enhancing the energy harvesting performance is examined through numerical simulations. The results demonstrate that hybrid trajectories applied to a two-flap wing configuration outperform a single flat plate and a wing with leading and trailing flaps both operating under a sinusoidal trajectory. The wing length spans from 45% to 55%, with the leading flap length ranging from 25% to 35%. The trailing flap lengths adjust accordingly to ensure the combined total matches the flat plate’s full length, which is 100%. The wing pitch angle was fixed at 85° while the leading flap’s pitch angle varied between 40° and 55° and the pitch angle of the trailing flap ranged from 0° to 20°. The findings reveal that utilizing hybrid motion on a wing fitted with leading and trailing flaps notably improves power output in comparison to configurations with either one plate or three plates. The power output is achieved at particular dimensions: a leading flap length of 30%, a wing length of 55%, and a trailing flap length of 15%. The corresponding pitch angles are 50° for the leading flap, 85° for the wing, and 10° for the trailing flap. The aforementioned configuration results in a 34.06% increase in output power in comparison to one plate. The maximum efficiency for this setup reaches 44.21%. This underscores the superior performance of hybrid trajectories over sinusoidal trajectories in enhancing energy extraction performance. Full article
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21 pages, 4819 KiB  
Article
Methane/Air Flame Control in Non-Premixed Bluff Body Burners Using Ring-Type Plasma Actuators
by Fatemeh Bagherighajari, Mohammadmahdi Abdollahzadehsangroudi and José C. Páscoa
Actuators 2025, 14(2), 47; https://doi.org/10.3390/act14020047 - 22 Jan 2025
Viewed by 380
Abstract
Enhancing the combustion efficiency and flame stability in conventional systems is essential for reducing carbon emissions and advancing sustainable energy solutions. In this context, electrohydrodynamic plasma actuators offer a promising active control method for modifying and regulating flame characteristics. This study presents a [...] Read more.
Enhancing the combustion efficiency and flame stability in conventional systems is essential for reducing carbon emissions and advancing sustainable energy solutions. In this context, electrohydrodynamic plasma actuators offer a promising active control method for modifying and regulating flame characteristics. This study presents a numerical investigation into the effects of a ring-type plasma actuator positioned on the co-flow air side of a non-premixed turbulent methane/air combustion system—an approach not previously reported in the literature. The ring-type plasma actuator was designed by placing electrodes along the perimeter of the small diameter wall of the air duct. The impact of the plasma actuator on the reacting flow field within the burner was analyzed, with a focus on its influence on the flow dynamics and flame structure. The results, visualized through velocity and temperature contours, as well as flow streamlines, provide insight into the actuator’s effect on flame behavior. Two operating modes of the plasma actuators were evaluated: co-flow mode, where the aerodynamic effect of the plasma actuators was directed downstream; and counter-flow mode, where the effects were directed upstream. The findings indicate that the co-flow actuation positively reduces the flame height and enhances the flame anchoring at the root, whereas counter-flow actuation slightly weakens the flame root. Numerical simulations further revealed that co-flow actuation marginally increases the energy release by approximately 0.13%, while counter-flow actuation reduces the energy release by around 7.8%. Full article
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24 pages, 10928 KiB  
Article
Three-Dimensional Pulsating Flow Simulation in a Multi-Point Gas Admission Valve for Large-Bore CNG Engines
by Soo-Jin Jeong and Seong-Joon Moon
Actuators 2024, 13(12), 492; https://doi.org/10.3390/act13120492 - 2 Dec 2024
Viewed by 485
Abstract
This study examines the dynamic fluid behavior of a PWM-controlled Solenoid-Operated Gas Admission Valve (SOGAV) for large-bore CNG engines using 3D Computational Fluid Dynamics (CFD) simulations with dynamic mesh techniques. The research focuses on the influence of orifice geometry variations in the multi-hole [...] Read more.
This study examines the dynamic fluid behavior of a PWM-controlled Solenoid-Operated Gas Admission Valve (SOGAV) for large-bore CNG engines using 3D Computational Fluid Dynamics (CFD) simulations with dynamic mesh techniques. The research focuses on the influence of orifice geometry variations in the multi-hole restrictor and pressure differentials between the inlet and outlet on flow stability, turbulence, and valve performance. Results demonstrate that multi-hole restrictors with different-sized orifices improve flow uniformity and reduce turbulence, thereby mitigating flow resistance. Transient simulations further reveal standing wave formation and pressure wave interference, emphasizing that steady-state models cannot capture critical transient phenomena, such as accelerated and decelerated jet-like flows and flow separation. These findings provide key insights into SOGAV optimization, contributing to enhanced fuel efficiency and engine responsiveness, meeting the performance requirements of modern gas engines. Full article
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22 pages, 11914 KiB  
Article
Analysis of Dynamic Flow Loss of High Water-Based Emulsion Pump
by Lirong Wan, Yuang Yin, Zhiyuan Sun, Gaozuo Sun, Guoqing Qi and Ruwei Zhang
Actuators 2024, 13(12), 482; https://doi.org/10.3390/act13120482 - 28 Nov 2024
Viewed by 510
Abstract
The emulsion pump’s flow loss directly affects its performance and efficiency. However, the annular plunger chamber leakage and valve core hysteresis are challenging to avoid during operation. This study systematically investigated the impact of the annular gap in the plunger cavity on emulsion [...] Read more.
The emulsion pump’s flow loss directly affects its performance and efficiency. However, the annular plunger chamber leakage and valve core hysteresis are challenging to avoid during operation. This study systematically investigated the impact of the annular gap in the plunger cavity on emulsion pump performance. Using theoretical analysis and computational fluid dynamics methods, it explored the mechanism of the port valve hysteresis during discharge. The simulation results show that the leakage of the annular gap is proportional to the gap thickness and the inlet pressure and inversely proportional to the dynamic viscosity of the emulsion. With the increase of plunger eccentricity, the leakage increases slowly. The increase in the outlet diameter of the port valve will lead to more significant hysteresis of the valve core. The change of outlet pressure has little effect on the hysteresis and flow of the spool, and the response speed of the wing-guided bevel discharge valve is faster than that of the ordinary poppet valve. Considering the above factors, the flow distribution process of the emulsion pump can be accurately analyzed, providing a reference for pump optimization. Full article
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Planned Papers

The below list represents only planned manuscripts. Some of these manuscripts have not been received by the Editorial Office yet. Papers submitted to MDPI journals are subject to peer-review.

Title: Investigating the Power Extraction of applying Hybrid Pitching Motion on a Wing with Leading and Trailing Flaps
Authors: SULEIMAN AWAD SULEIMAN SALEH; and Chang−Hyun Sohn
Affiliation: School of Mechanical Engineering, Kyungpook National University, Daegu 41566, South Korea.
Abstract: This research utilized a hybrid trajectory on a wing incorporating a dual flap with the goal of enhancing performance. The hybrid profiles initiate with a non−sinusoidal pattern during the interval 0.0 ≤ t/T ≤ 0.25, evolving toward a sinusoidal pattern within the range 0.25 < t/T ≤ 0.5. Similarly, hybrid motion follows a non−sinusoidal pattern in the range 0.5 < t/T ≤ 0.75, before shifting back to a sinusoidal pattern within the range 0.75 < t/T ≤ 1.0. The effectiveness of using hybrid trajectory on a wing with leading and trailing flaps in enhancing the energy harvesting performance is examined through numerical simulations. The results demonstrate that hybrid trajectories applied to a two−flap wing configuration outperform a single flat plate and a wing with leading and trailing flaps both operating under a sinusoidal trajectory. The wing length spans from 45% to 55%, with the leading flap length ranging from 25% to 35%. The trailing flap lengths adjust accordingly to ensure the combined total matches the flat plate's full length, which is 100%. The wing pitch angle was fixed at 85° while the leading flap's pitch angle varying between 40° and 55°, and the pitch angle of the trailing flap ranging from 0° to 20°. The findings reveal that utilizing hybrid motion on a wing fitted with leading and trailing flaps notably improves power output in comparison to configurations with either one plate or three plates. The power output is achieved at particular dimensions: a leading flap length of 30%, a wing length of 55%, and a trailing flap length of 15%. The corresponding pitch angles are 50° for the leading flap, 85° for the wing, and 10° for the trailing flap. The aforementioned configuration results in a 34.06% increase in output power in comparison to one plate and a 4.53% improvement in comparison to a wing with a two−flaps. The maximum efficiency for this setup reaches 44.21%. This underscores the superior performance of hybrid trajectories over sinusoidal trajectories in enhancing energy extraction performance.

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