Parametric Analysis and Design Optimization of a Loudspeaker-Driven Synthetic Jet Actuator Using Response Surface Model in Quiescent Conditions

Synthetic jet actuators (SJAs) are devices that control fluid flow by synthesizing surrounding fluid without altering the flow from the cavity. Before optimization, the selected diaphragm frequencies are subjected to a CFD solution using a dynamic mesh. Output parameters of selected loudspeaker-driven SJA are optimized under quiescent conditions. Comparisons are made between the best optimization candidate design point, experimental reference, and baseline CFD study before optimization. Re increases by 17% at 50[Formula: see text]Hz and 8.7% at other frequencies. St decreases by almost 30% across all frequencies. [Formula: see text] is maximized and held over 4. Optimized design, based on response surface model, demonstrated a consistent ability to produce higher, more centralized velocity profiles.

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Publication Details

Journal
International Journal of Computational Methods
Published
2024-10-18
DOI
https://doi.org/10.1142/s0219876224500683
Citations
1
Primary Topic
Plasma and Flow Control in Aerodynamics
Type
article
Field-Weighted Citation Impact
1.30

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article

Parametric Analysis and Design Optimization of a Loudspeaker-Driven Synthetic Jet Actuator Using Response Surface Model in Quiescent Conditions

Emre Kara
1 citations
International Journal of Computational Methods
Plasma and Flow Control in Aerodynamics
1.30
article

Parametric Analysis and Design Optimization of a Loudspeaker-Driven Synthetic Jet Actuator Using Response Surface Model in Quiescent Conditions

Emre Kara
article en
1 citations

Abstract

Synthetic jet actuators (SJAs) are devices that control fluid flow by synthesizing surrounding fluid without altering the flow from the cavity. Before optimization, the selected diaphragm frequencies are subjected to a CFD solution using a dynamic mesh. Output parameters of selected loudspeaker-driven SJA are optimized under quiescent conditions. Comparisons are made between the best optimization candidate design point, experimental reference, and baseline CFD study before optimization. Re increases by 17% at 50[Formula: see text]Hz and 8.7% at other frequencies. St decreases by almost 30% across all frequencies. [Formula: see text] is maximized and held over 4. Optimized design, based on response surface model, demonstrated a consistent ability to produce higher, more centralized velocity profiles.

International Journal of Computational MethodsVol. 22(05)
Gaziantep University (TR)
Ulusal Yüksek Başarımlı Hesaplama Merkezi, Istanbul Teknik Üniversitesi, Gaziantep Üniversitesi
Affordable and clean energy
Openalex Percentile: Top 12%
Plasma and Flow Control in Aerodynamics
1.30
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Parametric Analysis and Design Optimization of a Loudspeaker-Driven Synthetic Jet Actuator Using Response Surface Model in Quiescent Conditions — Emre Kara · International Journal of Computational Methods (2024) | TGRS Research Map | TGRS