Piece
Renumbered as AVIA 28/2383
Catalogue reference: AVIA 28/2942
Date: 1942
Renumbered as AVIA 28/2383
Piece
Effect of trailing edge thickness on blade loss and turbine stage efficiency: experiments
Catalogue reference: AVIA 28/3801
What’s it about?
This record is about the Effect of trailing edge thickness on blade loss and turbine stage efficiency: experiments dating from 1964 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 28/3801
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Date (When the record was created)
- 1964
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Description (What the record is about)
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Effect of trailing edge thickness on blade loss and turbine stage efficiency: experiments
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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)
- R264
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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/C4645926/
How to order it
- 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.
Catalogue hierarchy
Over 27 million records
This record is held at The National Archives, Kew
96,520 records
Within the department: AVIA
Records created or inherited by the Ministry of Aviation and successors, the Air...
4,056 records
Within the series: AVIA 28
Ministry of Aviation and predecessors: National Gas Turbine Establishment and predecessors:...
You are currently looking at the piece: AVIA 28/3801
Effect of trailing edge thickness on blade loss and turbine stage efficiency: experiments
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