يعرض 1 - 3 نتائج من 3 نتيجة بحث عن '"METHODE AUX FRONTIERES IMMERGEES"', وقت الاستعلام: 1.12s تنقيح النتائج
  1. 1
    Evaluation numérique des effets de confinement acoustique de bruit de fan dans une soufflerie en veine fermée

    المؤلفون: Thomas Le Garrec, Mathieu Lorteau

    المساهمون: DAAA, ONERA, Université Paris-Saclay [Châtillon], ONERA-Université Paris-Saclay

    المصدر: AIAA AVIATION Forum
    AIAA AVIATION Forum, Aug 2021, Virtuel, United States

    مصطلحات موضوعية: [PHYS]Physics [physics], 020301 aerospace & aeronautics, AEROACOUSTIQUE, METHODE AUX FRONTIERES IMMERGEES, Numerical assessment, 02 engineering and technology, Fan noise, 01 natural sciences, 7. Clean energy, Immersed Boundary Method, 010305 fluids & plasmas, fan noise, [SPI]Engineering Sciences [physics], 0203 mechanical engineering, 0103 physical sciences, Aeroacoustics, EFFETS DE CONFINEMENT ACOUSTIQUE, BRUIT DE FAN, acoustic confinement effects, CAA, Geology, Wind tunnel, Marine engineering

    URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5f0bbba114023d6f68befe31f58945ee
    https://doi.org/10.2514/6.2021-2302

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  2. 2
    Etude numérique, avec validation expérimentale, des effets d'installation du bruit de fan en configuration Over-Wing Nacelle à partir de la méthode aux frontières immergées

    المؤلفون: Stanislav L. Denisov, Victor Kopiev, Mathieu Lorteau, Ludovic Wiart

    المساهمون: DAAA, ONERA, Université Paris-Saclay (COmUE) [Châtillon], ONERA-Université Paris Saclay (COmUE), DAAA, ONERA, Université Paris Saclay (COmUE) [Meudon], ONERA-Université Paris-Saclay, Central Aerohydrodynamic Institute (TSAGI), Central Aerohydrodynamic Institute

    المصدر: 25th AIAA/CEAS Aeroacoustics Conference
    25th AIAA/CEAS Aeroacoustics Conference, May 2019, DELFT, Netherlands. ⟨10.2514/6.2019-2519⟩

    مصطلحات موضوعية: [PHYS]Physics [physics], 020301 aerospace & aeronautics, Wing, MASQUAGE ACOUSTIQUE, FAN NOISE, Computer science, Nacelle, Acoustics, AEROACOUSTIQUE, IMMERSERD BOUDARY METHOD, METHODE AUX FRONTIERES IMMERGEES, AEROACOUSTICS, 02 engineering and technology, Experimental validation, Fan noise, Immersed boundary method, 01 natural sciences, 7. Clean energy, ACOUSTIC SHIELDING, 010305 fluids & plasmas, [SPI]Engineering Sciences [physics], 0203 mechanical engineering, 0103 physical sciences, BRUIT DE FAN, CAA

    URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c36f777632484b10ffa32c3d15f3ff12
    https://hal.archives-ouvertes.fr/hal-02196627/document

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  3. 3
    Numerical study, with experimental validation, of fan noise installation effects in Over-Wing Nacelle configuration using the Immersed Boundary Method

    المؤلفون: Lorteau, Mathieu, Wiart, Ludovic, Kopiev, Victor

    المساهمون: DAAA, ONERA, Université Paris-Saclay (COmUE) [Châtillon], ONERA-Université Paris Saclay (COmUE), DAAA, ONERA, Université Paris Saclay (COmUE) [Meudon], ONERA-Université Paris-Saclay, Central Aerohydrodynamic Institute (TSAGI), Central Aerohydrodynamic Institute

    المصدر: 25th AIAA/CEAS Aeroacoustics Conference
    25th AIAA/CEAS Aeroacoustics Conference, May 2019, DELFT, Netherlands. ⟨10.2514/6.2019-2519⟩

    مصطلحات موضوعية: [PHYS]Physics [physics], [SPI]Engineering Sciences [physics], MASQUAGE ACOUSTIQUE, FAN NOISE, AEROACOUSTIQUE, IMMERSERD BOUDARY METHOD, METHODE AUX FRONTIERES IMMERGEES, AEROACOUSTICS, BRUIT DE FAN, ACOUSTIC SHIELDING, CAA

    URL الوصول: https://explore.openaire.eu/search/publication?articleId=od_______212::5a9b77e349ad57e56d8177d95b16dda6
    https://hal.archives-ouvertes.fr/hal-02196627/document

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