NASA NTRS · 19890009996
Duct flow nonuniformities for Space Shuttle Main Engine (SSME)
Abstract
Analytical capabilities for modeling hot gas flow on the fuel side of the Space Shuttle Main Engines are developed. Emphasis is placed on construction and documentation of a computational grid code for modeling an elliptical two-duct version of the fuel side hot gas manifold. Computational results for flow past a support strut in an annular channel are also presented.
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1988-06-30. Duct flow nonuniformities for Space Shuttle Main Engine (SSME). https://ntrs.nasa.gov/citations/19890009996
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