Solid Inflammability Boundary at Low Speed (SIBAL)This research program is concerned with the effect of low-speed, concurrent flow on the spreading and extinction processes of flames over solid fuels. The primary objective is to verify the theoretically predicted extinction boundary, using oxygen percentage and flow velocity as coordinates. In particular, we are interested in the low-speed quenching limits and the existence of the critical oxygen flammability limit. Detailed flame spread characteristics, including flame spread rate, flame size, and flame structure are sought. Since the predicted flame behavior depends on the inclusion of flame and surface radiation, the measured results will also be used to assess the importance of radiative heat transfer by direct comparison to a comprehensive numerical model. This project passed the Science Concept Review (SCR) in 1996. As a result, the experiment continues on the flight definition path, and is currently scheduled to be performed in the Space Station Combustion Integrated Rack (CIR). We present an overview of recent and ongoing work, including selected experimental and theoretical topics.
Document ID
19990053968
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
James S T'ien (Case Western Reserve University Cleveland, United States)
Paul Ferkul (National Center for Microgravity Research Cleveland, United States)
Kurt R Sacksteder (Glenn Research Center Cleveland, United States)
Hsin-Yi Shih (Case Western Reserve University Cleveland, United States)
Hasan Bedir (Case Western Reserve University Cleveland, United States)
Paul S Greenberg (Glenn Research Center Cleveland, United States)
Richard D Pettegrew (National Center for Microgravity Research Cleveland, OH United States)
Nancy Piltch (Glenn Research Center Cleveland, United States)
David Frate (Glenn Research Center Cleveland, United States)
Date Acquired
August 19, 2013
Publication Date
May 18, 1999
Publication Information
Publication: Fifth International Microgravity Combustion Workshop
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Propulsion and Power
Report/Patent Number
NASA/CP-1999-208917
Meeting Information
Meeting: 5th International Microgravity Combustion Workshop