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| dc.contributor.author | J. K. Harvey | en_US |
| dc.contributor.author | R. W. Jeffery | en_US |
| dc.contributor.author | D. C. Uppington | en_US |
| dc.date.accessioned | 2014-10-21T15:50:43Z | |
| dc.date.available | 2014-10-21T15:50:43Z | |
| dc.date.issued | 1971 | en_US |
| dc.identifier.other | ARC/R&M-3701 | en_US |
| dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/2976 | |
| dc.description.abstract | This report describes the design and development of a graphite-heated, continuous running, Mach 20 windtunnel which operates with Reynolds numbers between 6 x 10power4 and 5 x 10power6 per metre. Preliminary calibrations are presented for a contoured and a conical nozzle and for the performance of the centrebody diffuser. An electron beam probe is used to measure test section conditions. | en_US |
| dc.relation.ispartofseries | Aeronautical Research Council Reports & Memoranda | en_US |
| dc.title | The imperial college graphite heated hypersonic windtunnel | en_US |
