NASA NTRS · 19670000414
Computer program provides steady state analysis for liquid propellant propulsion systems
Abstract
Computer program uses Bernoullis formula and Newton-Raphson method to provide steady state fluid flow analysis of line pressure drop in a system with six outlets for each of two main storage tanks. Program flexibility arises in the ease with which changes in the fluid line geometry can be made.
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Clark, R. L.. 1967-11-01. Computer program provides steady state analysis for liquid propellant propulsion systems. https://ntrs.nasa.gov/citations/19670000414
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