| dc.creator | Young, A. D. | |
| dc.date | 2015-09-14T13:45:08Z | |
| dc.date | 2015-09-14T13:45:08Z | |
| dc.date | 1948-10 | |
| dc.date.accessioned | 2022-05-09T10:17:29Z | |
| dc.date.available | 2022-05-09T10:17:29Z | |
| dc.identifier | http://dspace.lib.cranfield.ac.uk/handle/1826/9439 | |
| dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/4842 | |
| dc.language | en | |
| dc.publisher | College of Aeronautics | |
| dc.relation | 14 addenda | |
| dc.relation | COA/14 | |
| dc.title | Note on the limits to the local Mach number on an aerofoil in subsonic flow | |
| dc.type | Report |
| Files | Size | Format | View |
|---|---|---|---|
| COA_Report_14_addenda_October_1948.pdf | 523.3Kb | application/pdf |
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