Investigation of hypersonic nozzle flow uniformity using NO fluorescence
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O'Byrne, Sean; Danehy, P; Houwing, A Frank
Description
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.
Collections | ANU Research Publications |
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Date published: | 2006 |
Type: | Journal article |
URI: | http://hdl.handle.net/1885/85116 |
Source: | Shock Waves |
DOI: | 10.1007/s00193-006-0013-6 |
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File | Description | Size | Format | Image |
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01_O'Byrne_Investigation_of_hypersonic_2006.pdf | 251.27 kB | Adobe PDF | Request a copy |
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