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: 20 June 2024 | Viewed by 2663

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
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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

Manuscript Submission Information

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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.

Published Papers (1 paper)

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Review

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 2 | Viewed by 2003
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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