Piece
See AVIA 6/10425
Catalogue reference: AVIA 6/40425
See AVIA 6/10425
Piece
Some examples of the calculated effect of angle of sweep and taper on the lift distribution...
Catalogue reference: AVIA 6/23488
What’s it about?
This record is about the Some examples of the calculated effect of angle of sweep and taper on the lift distribution... dating from 1952 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?
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 6/23488
-
Date (When the record was created)
- 1952
-
Description (What the record is about)
-
Some examples of the calculated effect of angle of sweep and taper on the lift distribution of a wing
-
Held by (Who holds the record)
- The National Archives, Kew
-
Former department reference (Former identifier given by the originating creator)
- Technical Note No Aero2202
-
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/C4750728/
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 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
96,954 records
27,068 records
You are currently looking at the piece: AVIA 6/23488
Some examples of the calculated effect of angle of sweep and taper on the lift distribution...
Related records
Records that share similar topics with this record.