Zobrazeno 1 - 10 of 10 pro vyhledávání: '"Matthieu Parenteau"'
2
Development of Parallel CFD Applications on Distributed Memory with Chapel
Autor: Matthieu Parenteau, Eric Laurendeau, Frédéric Plante, Simon Bourgault-Cote
Publikováno v: IPDPS Workshops
Traditionally, Computational Fluid Dynamics (CFD) software uses Message Passing Interface (MPI) to handle the parallelism over distributed memory systems. For a new developer, such as a student or a new employee, the barrier of entry can be high and
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::ec89a3eab9eaa862f9ceaeb572214854
https://doi.org/10.1109/ipdpsw50202.2020.00110
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3
Nonlinear Frequency-Domain Solver for Vortex Lattice Method
Autor: Matthieu Parenteau, Eric Laurendeau
Publikováno v: AIAA Journal. 56:2242-2251
This Paper presents a nonlinear frequency-domain solver for the vortex lattice method. Assuming a periodic solution, the wing circulation is represented in time by a Fourier series without the assu...
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::4faae6cfcb9c4e9259489030991315c1
https://doi.org/10.2514/1.j056704
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4
A transonic, viscous nonlinear frequency domain Vortex Lattice Method for aeroelastic analyses
Autor: Matthieu Parenteau, Eric Laurendeau
Publikováno v: Journal of Fluids and Structures. 107:103406
The Unsteady Vortex Lattice Method has interesting capabilities for nonlinear subsonic aeroelastic analyses. This paper aims to develop an aeroelastic framework based on the UVLM that is suitable for compressible, transonic and viscous unsteady flows
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::8f29c0e2eb9116c0a93c10458689f91a
https://doi.org/10.1016/j.jfluidstructs.2021.103406
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6
A general modal frequency-domain vortex lattice method for aeroelastic analyses
Autor: Matthieu Parenteau, Eric Laurendeau
Publikováno v: Journal of Fluids and Structures. 99:103146
The generalized aerodynamic force (GAF) matrix is derived for the Unsteady Vortex Lattice Method (UVLM) without the assumption of out-of-plane dynamics. As a result, the approach naturally includes in-plane motion and forces unlike the doublet lattic
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::f4b214ee1e69a2029f108a8fae563217
https://doi.org/10.1016/j.jfluidstructs.2020.103146
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8
Combined high-speed and high-lift wing aerodynamic optimization using a coupled VLM-2.5D RANS approach
Autor: Eric Laurendeau, Gerald Carrier, Matthieu Parenteau
Publikováno v: Aerospace Science and Technology
Aerospace Science and Technology, Elsevier, 2018, 76, pp.484-496. ⟨10.1016/j.ast.2018.02.023⟩
The paper presents a numerical framework for the aerodynamic analysis of aircraft wings in transonic cruise and take-off/landing compatible with preliminary and conceptual design phase requirements based on the Non-Linear Vortex Lattice Method (NL-VL
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c3b70aa5871655d3cbb644b8f4626651
https://hal.archives-ouvertes.fr/hal-02906126
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