NASA NTRS · 19730035174
Multiple-orifice liquid injection into hypersonic air streams.
Abstract
Review of oblique water and fluorocarbon injection test results obtained in experimental studies of the effects of multiple-orifice liquid injection into hypersonic air streams. The results include the finding that maximum lateral penetration from such injections increases linearly with the square root of the jet-to-freestream dynamic-pressure ratio and is proportional to an equivalent orifice diameter.
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Weaver, W. L.. 1972-12-01. Multiple-orifice liquid injection into hypersonic air streams.. https://ntrs.nasa.gov/citations/19730035174
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