NASA NTRS · 19950070436
Computer Hydrogen-Flow Splits In A Rocket Engine
Abstract
Report presents study of flows of hydrogen (as both coolant and fuel) along various paths in fuel injector of rocket engine. Study included computational simulations of flows.
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Romine, W. Dennis. 1995-11-01. Computer Hydrogen-Flow Splits In A Rocket Engine. https://ntrs.nasa.gov/citations/19950070436
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