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  • Luo, Bo  (4)
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  • 1
    Online Resource
    Online Resource
    World Scientific Pub Co Pte Ltd ; 2021
    In:  Modern Physics Letters B Vol. 35, No. 23 ( 2021-08-20), p. 2150384-
    In: Modern Physics Letters B, World Scientific Pub Co Pte Ltd, Vol. 35, No. 23 ( 2021-08-20), p. 2150384-
    Abstract: Unsteady flows in the field of engineering are usually calculated by the Unsteady Reynolds-Averaged Navier–Stokes (URANS) owing to the low requirements for computational efforts. However, the numerical resolution of URANS, especially in predicting the unsteady wake flows and sound, is still questionable. In this work, unsteady flow and sound calculations of a circular cylinder are carried out using Improved Delayed Detached Eddy Simulation (IDDES) and the Ffowcs Williams–Hawkings (FW-H) analogy. The predicted results of this calculation are compared with those from the previous studies in the literature in terms of the mean and RMS of the velocity components as well as the sound pressure. The results show that IDDES retains much of the numerical accuracy of the Large Eddy Simulation (LES) approach in predicting unsteady flows and noise while requiring a reduced computational resources in comparison to LES. It is believed that the IDDES can be applied to calculate the complex unsteady flows and flow generated sound with reasonable accuracy in engineering field, which can be used as a promising method for scale-resolving simulations to avoid the expensive computational requirements of LES.
    Type of Medium: Online Resource
    ISSN: 0217-9849 , 1793-6640
    RVK:
    Language: English
    Publisher: World Scientific Pub Co Pte Ltd
    Publication Date: 2021
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  • 2
    Online Resource
    Online Resource
    Elsevier BV ; 2020
    In:  Aerospace Science and Technology Vol. 98 ( 2020-03), p. 105700-
    In: Aerospace Science and Technology, Elsevier BV, Vol. 98 ( 2020-03), p. 105700-
    Type of Medium: Online Resource
    ISSN: 1270-9638
    Language: English
    Publisher: Elsevier BV
    Publication Date: 2020
    detail.hit.zdb_id: 2014638-3
    SSG: 16,12
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  • 3
    Online Resource
    Online Resource
    World Scientific Pub Co Pte Ltd ; 2023
    In:  Modern Physics Letters B Vol. 37, No. 03 ( 2023-01-30)
    In: Modern Physics Letters B, World Scientific Pub Co Pte Ltd, Vol. 37, No. 03 ( 2023-01-30)
    Abstract: The aerodynamic sound from bluff bodies is a practically important problem in various engineering applications. To control the aerodynamic noise, the sound emitted from a circular cylinder with and without a splitter plate in a Reynolds number (Re) of [Formula: see text] is studied using Ffowcs Williams and Hawkings (FW-H) acoustic analogy. The flow field is simulated by Detached Eddy Simulation (DES) approach to investigate the mechanism of the sound reduction using a splitter plate in a three-dimensional calculation. The predicted sound of the circular cylinder is compared with the experimental data from the literature, and a good agreement is achieved. The results from this study show that lift and drag fluctuations of the circular cylinder with the splitter plate are smaller than those of the no-splitter case. The Strouhal number related to vortex shedding with the splitter plate is slightly reduced compared to the unmodified circular cylinder due to the stretched shear layers. The pressure fluctuations in the wake are decreased by the splitter plate, resulting from the suppression of vortex shedding. The application of the splitter plate reduces the lift dipole which is the main sound source. It leads to a sound reduction of 13 dB.
    Type of Medium: Online Resource
    ISSN: 0217-9849 , 1793-6640
    RVK:
    Language: English
    Publisher: World Scientific Pub Co Pte Ltd
    Publication Date: 2023
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  • 4
    Online Resource
    Online Resource
    World Scientific Pub Co Pte Ltd ; 2021
    In:  Modern Physics Letters B Vol. 35, No. 16 ( 2021-06-10), p. 2150267-
    In: Modern Physics Letters B, World Scientific Pub Co Pte Ltd, Vol. 35, No. 16 ( 2021-06-10), p. 2150267-
    Abstract: The noise emitted from an axial fan has become one of the primary concerns for many industrial applications. This paper presents the work to predict the noise generation and investigate sound sources in a low speed axial fan. Computational fluid dynamics modeling is conducted using Scale Adaptive Simulation for the unsteady flow field. The sound predictions by the acoustic analogy are in good agreement with the experimental data. The results from this study show that the aerodynamic interaction between the blades and outlet vanes has a major contribution to the radiated noise spectrum. Two types of sources of narrowband humps are identified in the axial fan. The first is found at the leading edge of the blade tip, which is related to the interaction of coherent flow structures in the blade tip region. The second is found in the vicinity of the blade hub, which can be attributed to the recirculating flow and hub vortex. The noise below the frequency of 1500 Hz is mainly due to the blade-outlet vane aerodynamic interaction, manifested as the tonal sound at BPF and its harmonics, whereas above 1500 Hz the broadband component of sound is mainly related to the turbulent boundary layers.
    Type of Medium: Online Resource
    ISSN: 0217-9849 , 1793-6640
    RVK:
    Language: English
    Publisher: World Scientific Pub Co Pte Ltd
    Publication Date: 2021
    Location Call Number Limitation Availability
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