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    Exa Corporation

    企业
    339论文总数
    1.4万引用总数

    Exa Corporation was a developer and distributor of computer-aided engineering (CAE) software. Its main product was PowerFLOW, a lattice-boltzmann derived implementation of computational fluid dynamics (CFD), which can very accurately simulate internal and external flows in low-Mach regimes. PowerFLOW is used extensively in the international automotive and transportation industries.On November 17, 2017, Dassault Systèmes completed acquisition of Exa Corporation. Exa became part of Dassault's SIMULIA brand.

    论文量&引用量时间轴

    机构学者

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    Hudong Chen
    Hudong Chen
    College of Energy Engineering, Zhejiang University
    论文:83引用:0H-index:0
    Raoyang Zhang
    Raoyang Zhang
    Dassault Systèmes
    论文:32引用:0H-index:0
    David Freed
    David Freed
    Exa Corporation
    论文:32引用:0H-index:0
    Bradley D. Duncan
    Bradley D. Duncan
    Department of Electrical & Computer Engineering;University of Dayton;Department of Electrical & Computer Engineering, University of Dayton
    论文:25引用:0H-index:0
    Franck Perot
    Franck Perot
    Altair Engineering
    论文:24引用:0H-index:0
    Richard Shock
    Richard Shock
    Dassault Systèmes
    论文:21引用:0H-index:0
    Swen Noelting
    Swen Noelting
    Dassault Systemes Deutschland GmbH
    论文:17引用:0H-index:0
    Xiaowen Shan
    Xiaowen Shan
    Department of Mechanics and Aerospace Engineering, Southern University of Science and Technology
    论文:17引用:0H-index:0
    Damiano Casalino
    Damiano Casalino
    Aerodynamics, Wind Energy, Flight Performance and Propulsion, Faculty of Aerospace Engineering, Delft University of Technology
    论文:16引用:0H-index:0

    论文(339)

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    1Evaluation of a Public Program at the 28th Annual Conference of Occupational Health Professionals: Multiple Disciplines Considering the Importance of Occupational Health Nurses
    Satoru Kanamori,Mari Kusumoto, Chikako Shirata, Saori Yasukura, Noriko Tanaka,Wakana Harada
    2020SANGYO EISEIGAKU ZASSHI(2020)
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    2Very-Large Eddy Simulations of the M219 Cavity at High-Subsonic and Supersonic Conditions
    Simone Mancini,Alexander Kolb,Ignacio Gonzalez-Martino,Damiano Casalino
    2019AIAA Scitech 2019 Forum(2019)引用:11
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    3Simulation-Based Assessment of a Full-Scale Installed Quiet Landing Gear
    Benjamin M. Duda,Ryan Ferris,Mehdi R. Khorrami

    Full-scale simulations of a Gulfstream G-III aircraft, performed in support of the NASA Acoustic Research Measurements flights, are presented to complement results discussed in earlier studies. The flow solver employed in those studies, Dassault Systemes’ lattice Boltzmann PowerFLOW®, was also used during this investigation to conduct time-dependent simulations of the entire aircraft in landing configuration with a fully dressed landing gear. The high-fidelity simulations, performed at a Mach number of 0.23 and a Reynolds number of 10.5 × 106 based on mean aerodynamic chord, captured all relevant airframe noise sources. The computations were used to assess the aeroacoustic performance of the main landing gear, with and without noise reduction fairings installed, of a G-III aircraft equipped with Adaptive Compliant Trailing Edge technology and conventional Fowler flaps. To facilitate comparison of predicted noise signatures with effective perceived noise levels obtained from flight test measurements, the “as-flown” nose landing gear geometry, missing in our earlier studies, was added to the simulated G-III aircraft configurations. The high fidelity, synthetic data were post-processed using a Ffowcs-Williams and Hawkings integral approach to estimate farfield acoustic behavior, with pressures on the model solid surface or pressure and velocity components on a permeable surface enveloping the acoustic near field used as input.

    201925th AIAA/CEAS Aeroacoustics Conference(2019)引用:8
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    4Effects of Wall Modifications on Pressure Oscillations in High-Subsonic and Supersonic Flows over Rectangular Cavities
    Simone Mancini,Alexander Kolb,Ignacio Gonzalez-Martino,Damiano Casalino
    201925th AIAA/CEAS Aeroacoustics Conference(2019)引用:7
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    5Simulations of Chevrons on Single Flow Hot Jets
    Matthew L. Nickerson,Ryan Ferris, Wouter Cornelius Pieter van der Velden
    2019AIAA Scitech 2019 Forum(2019)引用:5
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