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Spot Radiative Ignition and Subsequent Three Dimensional Flame Spread Over Thin Cellulose FuelsSpontaneous radiative ignition and transition to flame spread over thin cellulose fuel samples was studied aboard the USMP-3 STS-75 Space Shuttle mission, and in three test series in the 10 second Japan Microgravity Center (JAMIC). A focused beam from a tungsten/halogen lamp was used to ignite the center of the fuel sample while an external air flow was varied from 0 to 10 cm/s. Non-piloted radiative ignition of the paper was found to occur more easily in microgravity than in normal gravity. Ignition of the sample was achieved under all conditions studied (shuttle cabin air, 21%-50% O2 in JAMIC), with transition to flame spread occurring for all but the lowest oxygen and flow conditions. While radiative ignition in a quiescent atmosphere was achieved, the flame quickly extinguished in air. The ignition delay time was proportional to the gas-phase mixing time, which is estimated using the inverse flow rate. The ignition delay was a much stronger function of flow at lower oxygen concentrations. After ignition, the flame initially spread only upstream, in a fan-shaped pattern. The fan angle increased with increasing external flow and oxygen concentration from zero angle (tunneling flame spread) at the limiting 0.5 cm/s external air flow, to 90 degrees (semicircular flame spread) for external flows at and above 5 cm/s, and higher oxygen concentrations. The fan angle was shown to be directly related to the limiting air flow velocity. Despite the convective heating from the upstream flame, the downstream flame was inhibited due to the 'oxygen shadow' of the upstream flame for the air flow conditions studied. Downstream flame spread rates in air, measured after upstream flame spread was complete and extinguished, were slower than upstream flame spread rates at the same flow. The quench regime for the transition to flame spread was skewed toward the downstream, due to the augmenting role of diffusion for opposed flow flame spread, versus the canceling effect of diffusion at very low cocurrent flows.
Document ID
20000070853
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Olson, Sandra L.
(NASA Glenn Research Center Cleveland, OH United States)
Kashiwagi, T.
(National Inst. of Standards and Technology Gaithersburg, MD United States)
Kikuchi, M.
(Tsukuba Space Center Ibaraki, Japan)
Fujita, O.
(Hokkaido Univ. Sapporo, Japan)
Ito, K.
(Hokkaido Univ. Sapporo, Japan)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Propellants And Fuels
Funding Number(s)
CONTRACT_GRANT: C-32001-R
PROJECT: RTOP 101-32-OB
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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