Zobrazeno 1 - 10
of 27
pro vyhledávání: '"Philippe Reulet"'
Publikováno v:
Energies, Vol 14, Iss 3, p 613 (2021)
The aerodynamic and thermal behaviour of multiperforated zones in combustors is essential to the development of future combustion chambers. Detailed databases are therefore crucial for the validation of RANS/LES solvers, but also regarding the deriva
Externí odkaz:
https://doaj.org/article/adad6f583fb24dfd9823c1564c4e0253
Autor:
Sacha Hirsch, Nicolas Fdida, Cornelia Irimiea, Sylvain Petit, Baptiste Dejean, Philippe Reulet, Benoît Fond, Guillaume Pilla
Publikováno v:
World Congress on Momentum, Heat and Mass Transfer.
Autor:
Arnulfo Carazo-Mendez, Fabien Mery, Philippe Reulet, Frank Simon, Estelle Piot, Delphine Sebbane
Publikováno v:
Journal of Aircraft
Journal of Aircraft, American Institute of Aeronautics and Astronautics, 2019, pp.1-13. ⟨10.2514/1.C035157⟩
Journal of Aircraft, American Institute of Aeronautics and Astronautics, 2019, pp.1-13. ⟨10.2514/1.C035157⟩
International audience; This study investigates the temperature effect on the impedance of conventional single degree-of-freedom liners, both without and with grazing flow. Experiments are performed in a controlled environment, with a detailed monito
Publikováno v:
Experiments in Fluids
Experiments in Fluids, Springer Verlag (Germany), 2021, 62 (4), pp.82. ⟨10.1007/s00348-021-03184-w⟩
Experiments in Fluids, Springer Verlag (Germany), 2021, 62 (4), pp.82. ⟨10.1007/s00348-021-03184-w⟩
International audience; The development of turbofans with larger fan diameters, shorter inlets, and thinner walls forces the acoustic liners to be placed closer to the hot parts of engines. This experimental study investigates the combined effects of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::036dc2ea6f4b0c39d91aa1c9aca9437d
https://hal.archives-ouvertes.fr/hal-03220702/document
https://hal.archives-ouvertes.fr/hal-03220702/document
Publikováno v:
Fire and Materials
Fire and Materials, Wiley-Blackwell, 2021, 45 (3), pp.435-447. ⟨10.1002/fam.2937⟩
Fire and Materials, Wiley-Blackwell, 2021, 45 (3), pp.435-447. ⟨10.1002/fam.2937⟩
International audience; Fire‐induced decomposition of composite materials involves complex and coupled multi‐physics phenomena experienced for instance in standard tests (cone calorimeter, FAR 25.856(b):2003 and ISO 2685:1998(e)). It is proposed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f83179e24ce3e5b4721d9b1ad31f8e50
https://hal.archives-ouvertes.fr/hal-03176102
https://hal.archives-ouvertes.fr/hal-03176102
Publikováno v:
Energies
Energies, MDPI, 2021, 14 (3), pp.613. ⟨10.3390/en14030613⟩
Volume 7A: Heat Transfer
ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. Volume 7A: Heat Transfer.
ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition
ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, Sep 2020, Virtual, United Kingdom. pp.GT2020-16311, ⟨10.1115/GT2020-16311⟩
Energies, Vol 14, Iss 613, p 613 (2021)
Energies, MDPI, 2021, 14 (3), pp.613. ⟨10.3390/en14030613⟩
Volume 7A: Heat Transfer
ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. Volume 7A: Heat Transfer.
ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition
ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, Sep 2020, Virtual, United Kingdom. pp.GT2020-16311, ⟨10.1115/GT2020-16311⟩
Energies, Vol 14, Iss 613, p 613 (2021)
The aerodynamic and thermal behaviour of multiperforated zones in combustors is essential to the development of future combustion chambers. Detailed databases are therefore crucial for the validation of RANS/LES solvers, but also regarding the deriva
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9d9ec5b31acc62df3fa548580f9940bd
https://hal.archives-ouvertes.fr/hal-03457828
https://hal.archives-ouvertes.fr/hal-03457828
Publikováno v:
International Journal of Heat and Fluid Flow
International Journal of Heat and Fluid Flow, Elsevier, 2020, 85, pp.108672. ⟨10.1016/j.ijheatfluidflow.2020.108672⟩
International Journal of Heat and Fluid Flow, Elsevier, 2020, 85, pp.108672. ⟨10.1016/j.ijheatfluidflow.2020.108672⟩
This work details an experimental investigation aiming at characterizing aerodynamic and heat transfer effects induced by roughness elements on a fully-rough zero-pressure-gradient turbulent boundary layer (TBL). The studied rough surfaces were compo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1090955e3288045b05977e79c4261dd1
https://hal.archives-ouvertes.fr/hal-02923751
https://hal.archives-ouvertes.fr/hal-02923751
Publikováno v:
SAE International Conference on Icing of Aircraft, Engines and Structures
SAE International Conference on Icing of Aircraft, Engines and Structures, Jun 2019, Minneapolis, United States. ⟨10.4271/2019-01-1935⟩
SAE International Conference on Icing of Aircraft, Engines and Structures, Jun 2019, Minneapolis, United States. ⟨10.4271/2019-01-1935⟩
International audience; In the framework of the SUNSET2 program, ice accretion numerical tools were assessed against experimental data. The database of ice shapes was generated on CRM-like swept-wings in NASA's IRT wind tunnel. This paper discusses c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bcb0033f99e521e0e034aa5f872575a5
https://hal.archives-ouvertes.fr/hal-02859982
https://hal.archives-ouvertes.fr/hal-02859982
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:
Quantitative InfraRed Thermography Journal. 6:225-248
In the context of the development of an efficient coupling method which improves aerothermal unsteady simulation accuracy, ONERA has achieved experimental validations based on a standard turbofan engine configuration. The objective of the present wor