| Download | - View final version: Flow and temperature distribution in the reheat tailpipe of Derwent VIII engine No. 10653 (PDF, 2.0 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003859 |
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| Author | Search for: Fowler, H. S.1 |
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| Affiliation | - National Research Council Canada. National Aeronautical Establishment
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| Format | Text, Memorandum |
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| Physical description | 5 p. |
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| Abstract | In order to evaluate thrust In flight, the reheated Meteor VT 196 has been fitted with a total pressure rake in the tailpipe. In order to correlate the readings on this rake with the mean pressure existing in the tailpipe, a series of temperature, pressure, and direction traverses was ma e across the tailpipe of a similar engine. These tests were carried out on the Derwent VIII engine used for reheat control development in Cell No. 2 in the Engine Laboratory. |
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| Publication date | 1955-02-21 |
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| Publisher | National Research Council Canada |
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| Series | |
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| Language | English |
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| Peer reviewed | No |
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| Identifier | NAE-149-5 |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | f5215cb6-8015-48bb-867c-e65c22c1798c |
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| Record created | 2025-11-10 |
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| Record modified | 2025-11-27 |
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