Piece
Renumbered as AVIA 28/2383
Catalogue reference: AVIA 28/2942
Date: 1942
Renumbered as AVIA 28/2383
Piece
High alternating stresses in blades of axial flow compressor: investigation
Catalogue reference: AVIA 28/3703
What’s it about?
This record is about the High alternating stresses in blades of axial flow compressor: investigation dating from 1954 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?
No, this record is not available online. However, you can order a copy. Other ways to view it.
Can I see it in person?
Yes, this record is held at The National Archives and is available to see in person. How to view it.
Full description and record details
-
Reference (The unique identifier to the record described, used to order and refer to it)
- AVIA 28/3703
-
Date (When the record was created)
- 1954
-
Description (What the record is about)
-
High alternating stresses in blades of axial flow compressor: investigation
-
Held by (Who holds the record)
- The National Archives, Kew
-
Former department reference (Former identifier given by the originating creator)
- R157
-
Legal status (A note as to whether the record being described is a Public Record or not)
- Public Record(s)
-
Closure status (Whether the record is ‘open’ (available to the public) or ‘closed’ (not available due to a legal exemption))
- Open Document, Open Description
-
Record URL
- https://beta.nationalarchives.gov.uk/catalogue/id/C4645528/
How to order it
- View this record page in our current catalogue
- Check viewing and downloading options
- Select an option and follow instructions
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
96,521 records
4,056 records
You are currently looking at the piece: AVIA 28/3703
High alternating stresses in blades of axial flow compressor: investigation
Related records
Records that share similar topics with this record.