NASA NTRS · 19620005077
Relation of Atomization and Rocket Combustor Performance
Abstract
Small initial drop-size distribution allows more rapid and complete vaporization and is related to combustion and exhaust velocity efficiency.
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Robert D. Ingebo. 1962-04-01. Relation of Atomization and Rocket Combustor Performance. https://ntrs.nasa.gov/citations/19620005077
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