Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Vincent Brion"'
The interaction of a line vortex with a collinearly aligned jet is a prototypical configuration for various important applications in aeronautics. The purpose of this study is to analyze the impact of the jet flow on the kinematics and dynamics of a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::89f996487386bc0ae88e6fce6625e983
https://doi.org/10.1063/5.0127634
https://doi.org/10.1063/5.0127634
Autor:
Rolando Cruz Marquez, Jean Claude Monnier, Geoffrey Tanguy, Marie Couliou, Vincent Brion, Patrick Dupont
Publikováno v:
AIAA AVIATION 2022 Forum.
Autor:
Vincent Brion, Marie Couliou, Jean Claude Monnier, Geoffrey Tanguy, Louis N. Cattafesta, Patrick Dupont, Rolando Cruz Marquez
Publikováno v:
AIAA AVIATION 2021 FORUM.
Publikováno v:
Journal of Fluid Mechanics. 866:399-430
We investigate optimal perturbation in the flow past a finite aspect ratio ($AR$) wing. The optimization is carried out in the regime where the fully developed flow is steady. Parametric study over time horizon ($T$), Reynolds number ($Re$), $AR$, an
Publikováno v:
STO-AVT-338-Specialists’Meeting on ‘Advanced Wind Tunnel Boundary Simulation'
STO-AVT-338-Specialists’Meeting on ‘Advanced Wind Tunnel Boundary Simulation', May 2021, Berlin, Germany
STO-AVT-338-Specialists’Meeting on ‘Advanced Wind Tunnel Boundary Simulation', May 2021, Berlin, Germany
International audience; Modern CFD techniques offer new opportunities to upgrade wind tunnels. Here we apply a RANS model to compute the flow through the circuit of the S3Ch transonic wind tunnel of ONERA Meudon center. The flow is set by implementin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::8a6441e9ebd626d4d1a6d95346481a96
https://hal.archives-ouvertes.fr/hal-03255343/document
https://hal.archives-ouvertes.fr/hal-03255343/document
Publikováno v:
Experiments in Fluids
Experiments in Fluids, Springer Verlag (Germany), 2020, 61 (126), pp.1-23. ⟨10.1007/s00348-020-02957-z⟩
Experiments in Fluids, 2020, 61 (126), pp.1-23. ⟨10.1007/s00348-020-02957-z⟩
Experiments in Fluids, Springer Verlag (Germany), 2020, 61 (126), pp.1-23. ⟨10.1007/s00348-020-02957-z⟩
Experiments in Fluids, 2020, 61 (126), pp.1-23. ⟨10.1007/s00348-020-02957-z⟩
International audience; Experimental analysis and modelling of the losses in the tip leakage flow of an isolated, non-rotating blade setup B. Deveaux · C. Fournis · V. Brion · J. Marty · A. Dazin Abstract Improving pressure rise capabilities of a
Publikováno v:
Journal of Fluid Mechanics
Journal of Fluid Mechanics, Cambridge University Press (CUP), 2020, 908, pp.29. ⟨10.1017/jfm.2020.898⟩
Journal of Fluid Mechanics, Cambridge University Press (CUP), 2020, 908, pp.29. ⟨10.1017/jfm.2020.898⟩
The present work investigates the excitation process by which free-stream disturbances are transformed into vortex-core perturbations. This problem of receptivity is modelled in terms of the resolvent in frequency space as the linear response to forc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5b04f724b8ee3b43e2d7355bd69b2fd1
https://hal.archives-ouvertes.fr/hal-03048005/file/DYNFLUID_JFM_2020_ROBINET.pdf
https://hal.archives-ouvertes.fr/hal-03048005/file/DYNFLUID_JFM_2020_ROBINET.pdf
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, SAGE Publications, 2020, 234 (1), pp.124-139. ⟨10.1177/0954410018824516⟩
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, SAGE Publications, 2020, 234 (1), pp.124-139. ⟨10.1177/0954410018824516⟩
International audience; An experimental investigation of the transonic flow past the laminar OALT25 airfoil has been conducted to analyze the impact of laminar flow upon the shock wave dynamics and the existence of a laminar buffet like phenomenon. T
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c18099c221e5b8a667e9fad62b27d97a
https://hal.archives-ouvertes.fr/hal-02612987/document
https://hal.archives-ouvertes.fr/hal-02612987/document
Publikováno v:
Journal of Fluid Mechanics
Journal of Fluid Mechanics, Cambridge University Press (CUP), 2018, 850, pp.156-178. ⟨10.1017/jfm.2018.470⟩
Journal of Fluid Mechanics, Cambridge University Press (CUP), 2018, 850, pp.156-178. ⟨10.1017/jfm.2018.470⟩
A large-eddy simulation of laminar transonic buffet on an airfoil at a Mach number $M=0.735$, an angle of attack $\unicode[STIX]{x1D6FC}=4^{\circ }$, a Reynolds number $Re_{c}=3\times 10^{6}$ has been carried out. The boundary layer is laminar up to
Publikováno v:
Journal of Fluid Mechanics
Journal of Fluid Mechanics, Cambridge University Press (CUP), 2019, 885, pp.A26-1-A26-26. ⟨10.1017/jfm.2019.1002⟩
Journal of Fluid Mechanics, Cambridge University Press (CUP), 2019, 885, pp.A26-1-A26-26. ⟨10.1017/jfm.2019.1002⟩
International audience; The dynamics and control of a vortex pair in ground effect are investigated ina planar, incompressible and laminar setting. The evolution of the vortices obtained numerically shows vortex rebound as a consequence of the separa