Piece
Renumbered as AVIA 28/2383
Catalogue reference: AVIA 28/2942
Date: 1942
Renumbered as AVIA 28/2383
Piece
W2 Mk 4 engine: effect of compressor temperature rise on performance and blade angle
Catalogue reference: AVIA 28/2923
What’s it about?
This record is about the W2 Mk 4 engine: effect of compressor temperature rise on performance and blade angle dating from 1941 in the series Ministry of Aviation and predecessors: National Gas Turbine Establishment and predecessors:.... It is held at The National Archives, Kew.
Is it available online?
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Full description and record details
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Reference (The unique identifier to the record described, used to order and refer to it)
- AVIA 28/2923
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Date (When the record was created)
- 1941
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Description (What the record is about)
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W2 Mk 4 engine: effect of compressor temperature rise on performance and blade angle
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Held by (Who holds the record)
- The National Archives, Kew
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Former department reference (Former identifier given by the originating creator)
- A 80
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Legal status (A note as to whether the record being described is a Public Record or not)
- Public Record(s)
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Closure status (Whether the record is ‘open’ (available to the public) or ‘closed’ (not available due to a legal exemption))
- Open Document, Open Description
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Record URL
- https://beta.nationalarchives.gov.uk/catalogue/id/C4645770/
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- View this record page in our current catalogue
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Series information
AVIA 28
Ministry of Aviation and predecessors: National Gas Turbine Establishment and predecessors:...
See the series level description for more information about this record.
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W2 Mk 4 engine: effect of compressor temperature rise on performance and blade angle
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