Zobrazeno 1 - 10
of 30
pro vyhledávání: '"Maxime Forte"'
Two separate experiments were conducted on a three-bladed NACA0012 rotor operating at a blade tip Reynolds number ranging from 44–110 ×103 using phase-locked infrared thermography (IRT) coupled with force and torque measurements. The first experim
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::91e0681ad1df2ea070517288dcd17629
https://oatao.univ-toulouse.fr/29666/
https://oatao.univ-toulouse.fr/29666/
Autor:
Jeanne Methel, Fabien Méry, Olivier Vermeersch, Maxime Forte, Gregory Delattre, Adrien Rouvière
In the present study, the effect of various twodimensional surface defects (forward-facing steps and ramps, backward-facing steps and ramps, gaps and steps-and-gaps) on boundary-layer transition was experimentally investigated in the transonic regime
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::44f0bfba37e166aac33dd5be95047307
https://doi.org/10.21203/rs.3.rs-2591458/v1
https://doi.org/10.21203/rs.3.rs-2591458/v1
Publikováno v:
Journal of Fluid Mechanics.
Experiments were conducted to study the transition and flow development in a laminar separation bubble (LSB) formed on an aerofoil. The effects of a wide range of free-stream turbulence intensity ( $0.15\,\%< Tu ) and streamwise integral length scale
Autor:
Fabien Méry, Jean-Luc Godard, Guillaume Arnoult, Philippe Bardoux, Christophe François, Maxime Forte, Estelle Piot
Publikováno v:
56th 3AF International Conference on Applied Aerodynamics
56th 3AF International Conference on Applied Aerodynamics, Mar 2022, Toulouse, France
HAL
56th 3AF International Conference on Applied Aerodynamics, Mar 2022, Toulouse, France
HAL
International audience; Reduction of the specific consumption of aircraft would lead to substantial economic and environmental benefits. A promising technique consists in reducing skin friction drag by delaying the laminar-turbulent transition point
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::c59ca1a73f8c8957ed22d59d07ddfe63
https://hal.science/hal-03716339
https://hal.science/hal-03716339
Publikováno v:
AIAA Journal
AIAA Journal, American Institute of Aeronautics and Astronautics, 2022, 60 (1), pp.508-519. ⟨10.2514/1.J060536⟩
AIAA Journal, American Institute of Aeronautics and Astronautics, 2021, 12 p. ⟨10.2514/1.J060536⟩
AIAA Journal, American Institute of Aeronautics and Astronautics, 2022, 60 (1), pp.508-519. ⟨10.2514/1.J060536⟩
AIAA Journal, American Institute of Aeronautics and Astronautics, 2021, 12 p. ⟨10.2514/1.J060536⟩
Articles in Advance; International audience; This paper investigates the effects of a porous wall on the development of Tollmien–Schlichting (TS) waves propagating inside a boundary layer. An experimental study performed in a low-speed wind tunnel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::994ce8df3543bcfc128daaed7c938d4d
https://hal.archives-ouvertes.fr/hal-03361895/file/DMPE21011_vacceptee.pdf
https://hal.archives-ouvertes.fr/hal-03361895/file/DMPE21011_vacceptee.pdf
Publikováno v:
Experimental Thermal and Fluid Science
Experimental Thermal and Fluid Science, Elsevier, 2022, 130, pp.110485. ⟨10.1016/j.expthermflusci.2021.110485⟩
Experimental Thermal and Fluid Science, Elsevier, 2022, 130, pp.110485. ⟨10.1016/j.expthermflusci.2021.110485⟩
An experimental investigation on the flow topology over a rotor operating atlow Reynolds numbers is presented. The feasibility of laminar to turbulenttransition experiments over small rotors is demonstrated. Phase-locked infraredthermography coupled
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::087037fab01479076f4b8505317934e6
https://hal.archives-ouvertes.fr/hal-03340224
https://hal.archives-ouvertes.fr/hal-03340224
Publikováno v:
Experiments in Fluids. 63
Wall suction is known to be an effective Laminar Flow Control (LFC) technique to delay laminar-turbulent transition, but its commercial implementation is still limited due to design and integration issues. In particular, current design tools that mod
Publikováno v:
IUTAM Laminar-Turbulent Transition ISBN: 9783030679019
IUTAM Laminar-Turbulent Transition
IUTAM Laminar-Turbulent Transition
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f71392f487a1c5066ba3308314f9da41
https://doi.org/10.1007/978-3-030-67902-6_18
https://doi.org/10.1007/978-3-030-67902-6_18
Publikováno v:
AIAA Scitech 2021 Forum
AIAA Scitech 2021 Forum, Jan 2021, Virtual event, United States. pp.AIAA 2021-0247, ⟨10.2514/6.2021-0247⟩
AIAA Scitech 2021 Forum, Jan 2021, Virtual event, United States. pp.AIAA 2021-0247, ⟨10.2514/6.2021-0247⟩
International audience; While it iswell known that increasing surface roughness tends to shift the transition location of a boundary-layer upstream, no model is currently able to accurately predict this shift as a function of the roughness parameters
Publikováno v:
Journal of Aircraft
Journal of Aircraft, American Institute of Aeronautics and Astronautics, 2018, 54 (2), pp.794-801. ⟨10.2514/1.C033647⟩
Journal of Aircraft, American Institute of Aeronautics and Astronautics, 2018, 54 (2), pp.794-801. ⟨10.2514/1.C033647⟩
International audience; Delaying laminar-turbulent transition is considered a crucial issue with respect to the reduction of airplanes environmental impact, allowing to reduce skin friction drag and thus, fuel consumption. As part of this thematic, b