Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Gillian Leplat"'
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:
Journal of Fire Sciences
Journal of Fire Sciences, SAGE Publications, 2016, 34 (5), p. 361-384. ⟨10.1177/0734904116653617⟩
Journal of Fire Sciences, SAGE Publications, 2016, 34 (5), p. 361-384. ⟨10.1177/0734904116653617⟩
International audience; Fire-induced decomposition of composite materials used for aircraft structures involves complex and coupled multi-physics phenomena studied through conventional standard tests such as cone calorimeter, FAR25.856(b):2003 and IS
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d35fe988ddef718185d901b5bfe87692
https://hal.archives-ouvertes.fr/hal-01401399
https://hal.archives-ouvertes.fr/hal-01401399
Publikováno v:
11th AIAA/ASME Joint Thermophysics and Heat Transfer Conference.
Carbon fibers/epoxy resin composite laminates decompose by pyrolysis and oxidation when submitted to high heat fluxes. A multi-components approach is proposed to describe all transient decompositions of the material from the virgin state to the final
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cdf7634fce92098935680d7b55241b3f
https://doi.org/10.2514/6.2014-2678
https://doi.org/10.2514/6.2014-2678
Publikováno v:
Volume 1: Heat Transfer in Energy Systems; Theory and Fundamental Research; Aerospace Heat Transfer; Gas Turbine Heat Transfer; Transport Phenomena in Materials Processing and Manufacturing; Heat and.
This study is dedicated to an innovative heatshield aeroshape intended to be the AEROFAST martian aerocapture demonstrator. The analysis of three representative Mars aerocapture trajectory points (maximum heat flux, maximum dynamic pressure and exit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f8edb8197c1144d8329edcd3151b92a
https://doi.org/10.1115/ht2012-58122
https://doi.org/10.1115/ht2012-58122
Publikováno v:
International Heat Transfer Conference
International Heat Transfer Conference, Aug 2010, Washington, United States
International Heat Transfer Conference, Aug 2010, Washington, United States
This study addresses the natural convection flow driven by a heated square cylinder within an air-filled enclosure for parameter values corresponding to the onset of unsteadiness and weakly transitional flow regime. 2D time-resolved PIV measurements
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::63757a67ede2f5a1ca9d564736e10483
https://hal.archives-ouvertes.fr/hal-01848855
https://hal.archives-ouvertes.fr/hal-01848855
Publikováno v:
Volume 2: Theory and Fundamental Research; Aerospace Heat Transfer; Gas Turbine Heat Transfer; Computational Heat Transfer.
A two-dimensional numerical analysis of a laminar natural convection flow within an air-filled enclosure is proposed in this paper from an unstable configuration previously studied experimentally. The flow is driven by a heated square-section cylinde
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fc86d0d30324cfc4a665152f053a4ad6
https://doi.org/10.1115/ht2009-88001
https://doi.org/10.1115/ht2009-88001
Publikováno v:
IUTAM Symposium on Flow Control and MEMS ISBN: 9781402068577
The purpose of this paper is to study experimentally the active control of separation on an ONERA D airfoil using micro-actuators. The configuration is a massively separated flow on the airfoil corresponding to a stalled case at R e =0.5 × 106 and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d5993a1be1016cbf7884f1785971a62d
https://doi.org/10.1007/978-1-4020-6858-4_24
https://doi.org/10.1007/978-1-4020-6858-4_24
Publikováno v:
Heat Transfer: Volume 3.
Consider an air-filled square cavity with cold top and bottom walls, adiabatic side walls and a centered heated sharp-edged source (a square-section cylinder). An unstable behavior has been highlighted previously while studying the effects of confine
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1473d58102e13b8c243a72a74f8bb03f
https://doi.org/10.1115/ht2008-56219
https://doi.org/10.1115/ht2008-56219
Autor:
Biasi, V.
Publikováno v:
Modélisation et simulation. INSTITUT SUPERIEUR DE L'AERONAUTIQUE ET DE L'ESPACE (ISAE), 2014. Français
Composite materials are increasingly used in new generation aircraft structures. Mass and as a consequence fuel savings encourage aircraft manufacturers to use them optimally. However, these materials can degrade quickly when exposed to significant h
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2592::1e884958bdaec6adf80c51dedd0db9dd
https://hal.archives-ouvertes.fr/tel-01234928/document
https://hal.archives-ouvertes.fr/tel-01234928/document
Autor:
Biasi, V.
Publikováno v:
Modélisation et simulation. INSTITUT SUPERIEUR DE L'AERONAUTIQUE ET DE L'ESPACE (ISAE), 2014. Français
Composite materials are increasingly used in new generation aircraft structures. Mass and as a consequence fuel savings encourage aircraft manufacturers to use them optimally. However, these materials can degrade quickly when exposed to significant h
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::1e884958bdaec6adf80c51dedd0db9dd
https://hal.archives-ouvertes.fr/tel-01234928
https://hal.archives-ouvertes.fr/tel-01234928