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High pressure droplet burning experiments in reduced gravityA parametric investigation of single droplet gasification regimes is helpful in providing the necessary physical ideas for sub-grid models used in spray combustion numerical prediction codes. A research program has been initiated at the LCSR to explore the vaporization regimes of single and interacting hydrocarbon and liquid oxygen droplets under high pressure conditions. This paper summarizes the status of the LCSR program on the high pressure burning of single fuel droplets; recent results obtained under normal and reduced gravity conditions with suspended droplets are presented. In the work described here, parabolic flights of the CNES Caravelle is used to create a reduced gravity environment of the order of 10(exp -2) g(sub O). For all the droplet burning experiments reported here, the suspended droplet initial diameters are scattered around 1.5 mm; and the ambient air temperature is 300 K. The ambient pressure is varied between 0.1 MPa and 12 MPa. Four fuels are investigated: methanol (Pc = 7.9 MPa), n-heptane (Pc = 2.74 MPa), n-hexane (Pc = 3.01 MPa) and n-octane (Pc = 2.48 MPa).
Document ID
19960008396
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chauveau, Christian
(Centre National de la Recherche Scientifique Orleans, France)
Goekalp, Iskender
(Centre National de la Recherche Scientifique Orleans, France)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Publication Information
Publication: NASA. Lewis Research Center, The 3rd International Microgravity Combustion Workshop
Subject Category
Materials Processing
Accession Number
96N15562
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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