NASA Technical Reports Server (NTRS) 19860014145: SSME fuelside preburner two-dimensional analysisReport as inadecuate



 NASA Technical Reports Server (NTRS) 19860014145: SSME fuelside preburner two-dimensional analysis


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The flow field within the fuelside preburner of the Space Shuttle Main Engine is calculated using a reacting flow code (REACT2D). Inlet and modeling parameters involved in the numerical calculation are systematically varied to establish the sensitivity of the calculated exit temperature profile. It is found that differences in the inlet equivalence

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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