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Turbine blade during thermal shock: design of analogue computer to determine temperature...

Catalogue reference: AVIA 28/2111

What’s it about?

This record is about the Turbine blade during thermal shock: design of analogue computer to determine temperature... dating from 1956 in the series Ministry of Aviation and predecessors: National Gas Turbine Establishment and predecessors:.... It is held at The National Archives, Kew.

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Full description and record details

Reference
AVIA 28/2111
Date
1956
Description

Turbine blade during thermal shock: design of analogue computer to determine temperature distribution

Held by
The National Archives, Kew
Former department reference
143
Legal status
Public Record(s)
Closure status
Open Document, Open Description
Record URL
https://beta.nationalarchives.gov.uk/catalogue/id/C4644094/

Series information

AVIA 28

Ministry of Aviation and predecessors: National Gas Turbine Establishment and predecessors:...

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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 28/2111

Turbine blade during thermal shock: design of analogue computer to determine temperature...

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