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Computational Active Flow and Noise Control

A special issue of Applied Sciences (ISSN 2076-3417). This special issue belongs to the section "Acoustics and Vibrations".

Deadline for manuscript submissions: closed (20 December 2024) | Viewed by 5854

Special Issue Editors


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Guest Editor
Department of Aerospace Engineering, Embry-Riddle Aeronautical University, Daytona Beach, FL 32114-3900, USA
Interests: computational fluid dynamics; computational aeroacoustics; flow control
Special Issues, Collections and Topics in MDPI journals

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Guest Editor
Department of Physical Sciences, Embry-Riddle Aeronautical University, Daytona Beach, FL 32114, USA
Interests: nonlinear control; robust control; adaptive control; nonlinear control application

Special Issue Information

Dear Colleagues,

The regulation control of airflow and noise is critically important for numerous applications, particularly those in aerospace, to alleviate the adverse effects of phenomena such as premature boundary-layer transition and stall, cavity flow oscillations, and flow–acoustic instabilities and limit cycle oscillations in aircraft wings and jet and fan noise, among others. In particular, it is estimated that the successful active flow control (AFC) of the boundary-layer transition on aircraft wings has the potential of saving billions of dollars through enhanced aerodynamic efficiency and an extended operational envelope for highly maneuverable aircrafts. While passive flow control approaches are actively utilized due to their relatively easy and inexpensive implementation, active, closed-loop AFC methods in particular may offer significant advantages by virtue of their capability to react in real time to the time-varying sensor measurements of flowfield properties. This enables closed-loop AFC and active noise control (ANC) systems to achieve continual flowfield and noise regulation in the presence of realistic time-varying operating conditions. Such technology generally involves sensors, actuators, and the controllers that have been carefully designed to achieve finite-time state estimation and asymptotic state regulation for a flow dynamic system, provided that a sufficient degree of flow control authority is available. Computationally, both open- and closed-loop AFC and ANC approaches present significant challenges due to the need to accurately resolve inherently unsteady, multi-scale physical phenomena, often involving unsteady fluid–structure interactions and the application of various closed-loop control approaches and reduced-order models. Hence, this Special Issue serves to provide a review and prospective for the state of the art in computational approaches that can be applied to active flow and noise control. Your contributions toward the issue are greatly appreciated. If you have any questions regarding the Special Issue, please feel free to contact the guest editor.

Prof. Dr. Vladimir V. Golubev
Dr. William MacKunis
Guest Editors

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Keywords

  • computational approaches
  • active flow control
  • active noise control
  • sensors and actuators
  • multi-scale phenomena, unsteady fluid–structure interactions
  • feedback-loop control methods
  • reduced-order models.

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Published Papers (3 papers)

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Research

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16 pages, 2591 KiB  
Article
Computation of Variable Noise Reduction System Efficiency for Supersonic Civil Aircraft During Takeoff
by Victor Kopiev, Ivan Belyaev and Sergey Velichko
Appl. Sci. 2025, 15(3), 1475; https://doi.org/10.3390/app15031475 - 31 Jan 2025
Viewed by 557
Abstract
The noise of next-generation supersonic civil aircraft can become a significant nuisance for the population in the vicinity of airports. This study investigates the efficiency of the noise control approach for a notional supersonic civil aircraft at takeoff, based on the implementation of [...] Read more.
The noise of next-generation supersonic civil aircraft can become a significant nuisance for the population in the vicinity of airports. This study investigates the efficiency of the noise control approach for a notional supersonic civil aircraft at takeoff, based on the implementation of a variable noise reduction system (VNRS) with thrust control. Noise levels are computed with a decoupling approach, where the engine noise data and the flight trajectory are calculated independently. It is shown that implementation of the VNRS for the supersonic civil aircraft could lead to a reduction in the certification noise levels at the lateral and flyover measurement points by about 4 EPNdB. The effect of VNRS on noise levels for two allowable positions of the lateral certification point (on the sideline and on the extended runway centerline) is considered and compared for the first time. It is found that the cumulative noise reduction at the flyover and lateral certification point due to the VNRS is larger by 0.8 EPNdB for the position of the lateral certification point on the sideline than for the position on the extended runway centerline. Full article
(This article belongs to the Special Issue Computational Active Flow and Noise Control)
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19 pages, 1696 KiB  
Article
Near-Field Aeroacoustics of Spanwise Forcing on a Transonic Wing: A DNS Study
by Niccolò Berizzi, Davide Gatti, Giulio Soldati, Sergio Pirozzoli and Maurizio Quadrio
Appl. Sci. 2025, 15(2), 814; https://doi.org/10.3390/app15020814 - 15 Jan 2025
Viewed by 790
Abstract
The transonic airflow around a supercritical wing with a shock wave is described via direct numerical simulations. Flow control for turbulent drag reduction is applied via streamwise traveling waves of spanwise velocity applied on a finite portion of the suction side. The near-field [...] Read more.
The transonic airflow around a supercritical wing with a shock wave is described via direct numerical simulations. Flow control for turbulent drag reduction is applied via streamwise traveling waves of spanwise velocity applied on a finite portion of the suction side. The near-field modifications caused by the forcing are studied via the analysis of the wake profile downstream of the trailing edge. Moreover, for the first time, the effects of spanwise forcing on aeroacoustic noise are considered to establish whether active flow control for drag reduction could possibly increase noise. By extracting the acoustic signals on a circumference placed in the near-field around the wing and by studying them in terms of sound intensity and frequency content, it is found that noise intensity is not significantly increased by spanwise forcing and that frequency content is only minimally altered. Furthermore, if the angle of attack is reduced to take into account the increased lift and the reduced drag made possible by the control action, changes in the noise characteristics become negligible. Full article
(This article belongs to the Special Issue Computational Active Flow and Noise Control)
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Review

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17 pages, 6610 KiB  
Review
Review of Control Technologies for Quiet Operations of Advanced Air-Mobility
by Samuel Afari, Vladimir Golubev, Anastasios S. Lyrintzis and Reda Mankbadi
Appl. Sci. 2023, 13(4), 2543; https://doi.org/10.3390/app13042543 - 16 Feb 2023
Cited by 8 | Viewed by 3428
Abstract
The current technologies for developing quiet rotor noise in urban canyons are reviewed. Several passive noise control approaches are discussed with their limitations in reducing both tonal and broadband noise. Blade tip modifications are seen to be one of the more successful in [...] Read more.
The current technologies for developing quiet rotor noise in urban canyons are reviewed. Several passive noise control approaches are discussed with their limitations in reducing both tonal and broadband noise. Blade tip modifications are seen to be one of the more successful in reducing tonal noise, with serrations at the trailing edge useful in reducing trailing edge broadband noise. Due to the adverse performance limitations of passive control, several optimization approaches are reviewed to discuss the possible improvements in performance of rotors. Additionally, a few legacy control technologies for helicopters are discussed. Active control technologies are investigated. The overall outlook and challenges to these methods are discussed with an eye on Advanced Air Mobility Vehicles (AAM). Full article
(This article belongs to the Special Issue Computational Active Flow and Noise Control)
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