Showing 81 - 100 results of 412 for search '"aeroacoustics"', query time: 0.16s Refine Results
  1. 81

    Aeroacoustic sound alteration in airway bronchoconstriction, represented by a constricted T-branch model by Gabriel Pramudita SAPUTRA, Kazunori NOZAKI, Satoshi II, Shigeo WADA

    Published 2015-01-01
    “…In the current study, an aeroacoustic investigation of sound generation in an airway model was performed experimentally to uncover the factors that change the sound characteristics due to bronchoconstriction. …”
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    Article
  2. 82

    Development and commissioning of an aeroacoustic test bench for the investigation of single and coaxial propeller noise by Gallo Erica, De Decker Julien, Bresciani Andrea, Haezebrouck Pauline, Garone Emanuele, Schram Christophe

    Published 2025-01-01
    “…This paper describes the design and commissioning of an aeroacoustic test rig for the study of single and coaxial propeller propulsive systems. …”
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    Turbomachinery Noise Review by Stéphane Moreau, Michel Roger

    Published 2024-03-01
    Subjects: “…aeroacoustics…”
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    Article
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    Cartesian Mesh Linearized Euler Equations Solver for Aeroacoustic Problems around Full Aircraft by Yuma Fukushima, Daisuke Sasaki, Kazuhiro Nakahashi

    Published 2015-01-01
    “…The linearized Euler equations (LEEs) solver for aeroacoustic problems has been developed on block-structured Cartesian mesh to address complex geometry. …”
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  14. 94

    Aeroacoustic Simulation for NASA CC3 Centrifugal Compressor Operating at off Design Condition by Alqaradawi Mohamed, Shahin Ibrahim, Gadala Mohamed, Badr Osama

    Published 2016-01-01
    “…The hub cavity flow effect on the compressor aeroacoustic generated noise is shown in the paper. The unsteady static pressure and sound pressure levels are compared not only at different location but also for design and off design operating points. …”
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    Comparative study of aeroacoustic performance of 1/8 and 1/1 pantographs coupled with cavity by Xiaoming Tan, Huifang Liu, Zhigang Yang, Hong Chen, Baojun Fu, Linli Gong

    Published 2024-07-01
    “…It is found that there is no direct scale similarity between their aeroacoustic performance. The 1/1 model airflow is separated at the leading edge of the panhead and reattached to the panhead, and its vortex shedding Strouhal number (St) is 0.17. …”
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