NASA NTRS · 20030064034
Shuttle Main Propulsion System LH2 Feed Line and Inducer Simulations
Abstract
This viewgraph presentation includes simulations of the unsteady flow field in the LH2 feed line, flow line, flow liner, backing cavity and inducer of Shuttle engine #1. It also evaluates aerodynamic forcing functions which may contribute to the formation of the cracks observed on the flow liner slots. The presentation lists the numerical methods used, and profiles a benchmark test case.
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Daniel Dorney, Jeffry Rothermel. Shuttle Main Propulsion System LH2 Feed Line and Inducer Simulations. https://ntrs.nasa.gov/citations/20030064034
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