S
Sanghyeon Kim
Researcher at Pusan National University
Publications - 18
Citations - 156
Sanghyeon Kim is an academic researcher from Pusan National University. The author has contributed to research in topics: Noise & Turbine. The author has an hindex of 5, co-authored 14 publications receiving 108 citations.
Papers
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Development of low noise drag-type vertical wind turbines
Sanghyeon Kim,Cheolung Cheong +1 more
TL;DR: In this paper, the aerodynamic noise characteristics of Savonius wind turbines were investigated using hybrid computational aero-acoustics techniques, and low-noise designs were proposed based on the understanding of the noise generation mechanism.
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Development of low-noise drag-type vertical wind turbines
Sanghyeon Kim,Cheolung Cheong +1 more
TL;DR: In this article, the aerodynamic noise characteristics of Savonius wind turbines were investigated using hybrid computational aero-acoustics techniques, and low-noise designs were proposed based on the understanding of the noise generation mechanism.
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Numerical investigation on cavitation flow of hydrofoil and its flow noise with emphasis on turbulence models
TL;DR: In this article, the effects of turbulence models on cavitation-flow patterns and the corresponding radiated sound waves are numerically investigated to characterize the effect of cavitation flow of hydrofoils.
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Numerical Investigation into Effects of Viscous Flux Vectors on Hydrofoil Cavitation Flow and Its Radiated Flow Noise
TL;DR: In this paper, the effects of viscous flux vectors on the predicted flow fields and its radiated noise were examined by comparing the hydro-dynamic forces, velocity distribution, volume fraction, far-field sound directivities, and sound spectrum of the three approaches.
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Investigation of flow and acoustic performances of suction mufflers in hermetic reciprocating compressor
TL;DR: In this paper, the authors investigated both the flow performance and the acoustic performance of a suction muffler by solving three-dimensional compressible Reynolds-averaged Navier-Stokes equations with high-order computational aero-acoustics schemes.