Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Fabien Gand"'
Autor:
Fabien Gand, Maxime Huet
Publikováno v:
Computers and Fluids
Computers and Fluids, Elsevier, 2021, 216, pp.104816. ⟨10.1016/j.compfluid.2020.104816⟩
Computers and Fluids, Elsevier, 2021, 216, pp.104816. ⟨10.1016/j.compfluid.2020.104816⟩
International audience; The present work is devoted to the assessment of a low-noise turbulence generation methodology used to produce boundary layer with three-dimensional resolved turbulence at the exit of a jet nozzle to reproduce experimental con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8aff35bc2bd1ad0fcbae7203ca0c4e27
https://hal.archives-ouvertes.fr/hal-03099618
https://hal.archives-ouvertes.fr/hal-03099618
Publikováno v:
AIAA Journal
AIAA Journal, American Institute of Aeronautics and Astronautics, 2017, page 1-19. ⟨10.2514/1.J055535⟩
AIAA Journal, American Institute of Aeronautics and Astronautics, 2017, page 1-19. ⟨10.2514/1.J055535⟩
International audience; This paper investigates the effect of turbulence injection using the random flow generation technique at the inlet boundaries of the core and fan channels of a dual-stream nozzle with an external plug. The objective is to repr
Autor:
Maxime Huet, Fabien Gand
Publikováno v:
25th AIAA/CEAS Aeroacoustics Conference.
Autor:
Fabien Gand
Publikováno v:
International Journal of Heat and Fluid Flow. 61:425-437
Hybrid RANS/LES simulations of two incompressible jets are performed with the Zonal Detached Eddy Simulation (ZDES). Two functioning modes of the ZDES for the selection of RANS and DES areas are evaluated, namely the user-defined mode (mode 1) and th
Publikováno v:
AIAA Journal. 54:3176-3190
This paper presents a study using zonal detached-eddy simulation to simulate the flow of a dual-stream nozzle. The nozzle design and operating conditions are typically those of an aircraft engine at cruise, although the external flow speed is not sim
Publikováno v:
AIAA Journal. 54:386-398
This study gives an insight into the corner flow around a wing mounted on a flat plate. Reynolds-averaged Navier–Stokes simulations and experimental data are compared for a Reynolds number based on the wing chord (Rec) equal to 3×105 and an angle
Autor:
Adrien Loseille, Weeded Ghedhaifi, Fabien Gand, Vivien Chmielarski, Vuillot François, Emmanuel Montreuil
Publikováno v:
2018 Atmospheric and Space Environments Conference.
Aircraft contrails may contribute to the global radiative forcing. In this context, the investigation of contrail formation in the near field of an aircraft may be helpful in developing strategies to reduce undesirable impacts. Contrail formation is
Publikováno v:
Progress in Hybrid RANS-LES Modelling ISBN: 9783319700304
This paper presents a comprehensive study of an impinging jet configuration (Grenson et al, Int J Heat Mass Trans 102:801–815, 2016), which has been selected for its high Reynolds number ReD = 60,000, small nozzle-to-plate distance H/D = 3 and temp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::570e69fe76b4a1c556661247a72849bb
https://doi.org/10.1007/978-3-319-70031-1_41
https://doi.org/10.1007/978-3-319-70031-1_41
Publikováno v:
AIAA Journal. 53:2869-2877
This study focuses on the corner flow separation occurring in a simplified wing-body junction composed of a NACA0015 twisted wing mounted on a flat plate at a Reynolds number based on the wing chord of Rec=1.2×106. Wind-tunnel test measurements are
Publikováno v:
23rd AIAA/CEAS Aeroacoustics Conference.