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Please use this identifier to cite or link to this item: http://hdl.handle.net/1842/2636

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Title: Microgravity Laminar Diffusion Flame In A Perpendicular Fuel And Oxidizer Streams Configuration
Authors: Brahmi, Lynda
Vietoris, Thomas
Rouvreau, Sebastien
Joulain, Pierre
David, L
Torero, Jose L
Issue Date: 2005
Citation: L. Brahmi, T. Vietoris, S. Rouvreau, P. Joulain L. David and J.L. Torero, Microgravity Laminar Diffusion Flame In A Perpendicular Fuel And Oxidizer Streams Configuration, AIAA Journal, 43, 8, 1725-1733, 2005.
Publisher: American Institute of Aeronautics and Astronautics
Abstract: Fuel is injected through a porous flat plate perpendicular to a stream of oxidizer flowing parallel to the surface of the burner for regimes corresponding to fire scenario in spacecrafts. Particle Image Velocimetry is used to characterize the flow structure in non-reactive conditions. The influence of fuel injection on the flow structure is evaluated and detailed description of the flow structure is presented. For combustion experiments, a minimum fuel injection velocity is shown to be necessary for a stable flame. The influence of thermal expansion on the flame is evaluated. A complementary numerical study is used to support the above experimental observations.
Description: Research paper published in the AIAA Journal 2005
Sponsor(s): European Space Agency
Centre National d’Etudes Spatiales and Minta Martin Research Fellowship
Keywords: spacecraft
fire safety
flow structure
thermal expansion, very low Reynolds
URI: http://hdl.handle.net/1842/2636
Appears in Collections:BRE Research Publications

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