Investigation of hypersonic nozzle flow uniformity using NO fluorescence
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O'Byrne, Sean
Danehy, P
Houwing, A Frank
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Springer
Abstract
Planar laser-induced fluorescence visualisation is used to investigate nonuniformities in the flow of a hypersonic conical nozzle. Possible causes for the nonuniformity are outlined and investigated, and the problem is shown to be due to a small step at the nozzle throat. Entrainment of cold boundary layer gas is postulated as the cause of the signal nonuniformity.
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Shock Waves
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2037-12-31
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