Flow Control Techniques: Advances in Flow System Analysis, Modeling and Applications

A special issue of Fluids (ISSN 2311-5521).

Deadline for manuscript submissions: 31 October 2024 | Viewed by 4129

Special Issue Editor


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Guest Editor
Department of Mechanical and Aerospace Engineering, Politecnico di Torino, 10129 Torino, Italy
Interests: flow control; computational fluid dynamics; compressor rotating stall; fluidic thrust vectoring; gasturbine design and control

Special Issue Information

Dear Colleagues,

Flow control is a fascinating topic of fluid dynamics that can play a key role in the route to the CO2-neutral growth of aviation transportation. The ambitious goals involved in this road map have pushed the designers towards aggressively optimized designs of flow devices and gas turbine components, which often become more prone to instabilities or abrupt performance losses in off-design conditions. 

Therefore, passive and active flow control strategies can enhance the performances of aerodynamic devices and increase safety margins both in subsonic and supersonic flight.

The key aspects of a flow control application are:

  1. The derivation of accurate real-time models of the nonlinear flow field. Substantial improvement on this topic may derive from recent advances in CFD simulations and experimental testing, that allow for a deeper understanding of flow unsteadiness and instabilities.
  2. The development of reliable flow manipulators and sensing systems, composed of a network of either physical or virtual sensors;
  3. The design of robust control laws, tailored to the specific system (e.g., by using the Digital Twin concept and Artificial Intelligence approaches) and to the targets of each flight mission phase. 

This Special Issue aims to collect the latest advances in the different techniques of passive and active flow control, including theoretical flow modeling, experimental investigations and numerical simulations of controlled/uncontrolled flow fields. Applications of classical approaches or artificial intelligence-based model reductions (e.g., by using deep learning, reinforced learning, and physically informed neural networks) are welcome.

Dr. Michele Ferlauto
Guest Editor

Manuscript Submission Information

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Keywords

  • trapped vortex
  • shock-wave control
  • drag reduction
  • high-lift profile
  • fluidic thrust vectoring
  • nozzle instabilities
  • dynamic stall
  • compressor rotating stall
  • synthetic jet
  • virtual shaping
  • plasma actuators
  • dielectric barrier discharge plasma actuator
  • combustion instability
  • supersonic inlets
  • scramjet

Published Papers (2 papers)

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Research

20 pages, 2113 KiB  
Article
Performance of DBD Actuator Models under Various Operating Parameters and Modifications to Improve Them
by Raul Alberto Bernal-Orozco, Ignacio Carvajal-Mariscal and Oliver Marcel Huerta-Chavez
Fluids 2023, 8(4), 112; https://doi.org/10.3390/fluids8040112 - 28 Mar 2023
Cited by 1 | Viewed by 1920
Abstract
Simulation is a valuable tool for the study of DBD actuators, therefore accurate, computationally efficient, and robust numerical models are required. The performance of three DBD actuator models was studied: the phenomenological Shyy and Suzen models, and the empirical Dörr and Kloker model. [...] Read more.
Simulation is a valuable tool for the study of DBD actuators, therefore accurate, computationally efficient, and robust numerical models are required. The performance of three DBD actuator models was studied: the phenomenological Shyy and Suzen models, and the empirical Dörr and Kloker model. The first objective of this work is to determine the ability of these models to reproduce the force and induced flow by comparing the numerical results with experimental reference data reported in the literature. As a second objective, modifications have been proposed to improve these models. Several simulations were performed in OpenFOAM with different geometrical parameters, voltages, and frequencies. Discrepancies and limitations of the models were identified. The modified Dörr and Kloker model allows more consistent use of this model by considering a factor that relates it to voltage and frequency. Shyy’s modified model reduces the overestimation of force and velocity. Suzen’s modified model is the one that fits the reference data better, so its use is suggested over the other models. The proposed modifications are easy to implement and allow significant improvements in the capacity of the models to reproduce the effects of a DBD actuator. Full article
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23 pages, 12564 KiB  
Article
Evaluation of Synthetic Jet Flow Control Technique for Modulating Turbulent Jet Noise
by Jairo Murillo-Rincón and Carlos Duque-Daza
Fluids 2023, 8(4), 110; https://doi.org/10.3390/fluids8040110 - 27 Mar 2023
Cited by 2 | Viewed by 1644
Abstract
The use of a synthetic jet as the flow control technique to modulate a turbulent incompressible round jet was explored and assessed by numerical simulations. The flow response was characterised in terms of turbulent statistics and acoustic response in the far-field. A quasi-Direct [...] Read more.
The use of a synthetic jet as the flow control technique to modulate a turbulent incompressible round jet was explored and assessed by numerical simulations. The flow response was characterised in terms of turbulent statistics and acoustic response in the far-field. A quasi-Direct Numerical Simulation (qDNS) strategy was used to predict the turbulent effects. The Ffowcs-Williams and Hawkings (FWH) acoustic analogy was employed to compute the far-field acoustic response. An amplification effect of the instabilities induced by the control jet was observed for some of the parameters explored. It was observed that the control technique allows controlling the axial distribution of the production and dissipation of turbulent kinetic energy, but with respect to the acoustic aspects, the appearance of a greater number of noise sources was observed, which in the far-field, resulted in an increase from 1 to 20 dB of the equivalent noise for the different operating parameters of the control technique studied. Full article
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