Piece
See AVIA 6/10425
Catalogue reference: AVIA 6/40425
See AVIA 6/10425
Piece
Development of wing flow technique of model testing at transonic speeds. part 2:...
Catalogue reference: AVIA 6/15218
What’s it about?
This record is about the Development of wing flow technique of model testing at transonic speeds. part 2:... dating from 1951 in the series Ministry of Defence and predecessors: Royal Aircraft Factory, later Royal Aircraft.... 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 6/15218
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Date (When the record was created)
- 1951
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Description (What the record is about)
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Development of wing flow technique of model testing at transonic speeds. part 2: further progress and tests up to M = 1.10 on a 60 deg sweptback wing (English Electric F23/49)
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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)
- TM Aero 214
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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/C4025539/
How to order it
- View this record page in our current catalogue
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- Select an option and follow instructions
Series information
AVIA 6
Ministry of Defence and predecessors: Royal Aircraft Factory, later Royal Aircraft...
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...
26,636 records
Within the series: AVIA 6
Ministry of Defence and predecessors: Royal Aircraft Factory, later Royal Aircraft...
You are currently looking at the piece: AVIA 6/15218
Development of wing flow technique of model testing at transonic speeds. part 2:...
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