Piece
Aerofoils: maximum lift; addendum to ARC 11084(DSIR 23/16921)
Catalogue reference: DSIR 23/17028
Date: 1948
Aerofoils: maximum lift; addendum to ARC 11084(DSIR 23/16921)
Piece
NACA 66 (215) - 216, 66, 1-212, and 65,-212 airfoils with 0.20 airfoil-chord split...
Catalogue reference: DSIR 23/14279
What’s it about?
This record is about the NACA 66 (215) - 216, 66, 1-212, and 65,-212 airfoils with 0.20 airfoil-chord split... dating from 1945 in the series Department of Scientific and Industrial Research: Aeronautical Research Council:.... It is held at The National Archives, Kew.
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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)
- DSIR 23/14279
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Date (When the record was created)
- 1945
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Description (What the record is about)
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NACA 66 (215) - 216, 66, 1-212, and 65,-212 airfoils with 0.20 airfoil-chord split flaps: wind tunnel investigation
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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)
- 8442
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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/C2428499/
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- View this record page in our current catalogue
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Series information
DSIR 23
Department of Scientific and Industrial Research: Aeronautical Research Council:...
See the series level description for more information about this record.
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You are currently looking at the piece: DSIR 23/14279
NACA 66 (215) - 216, 66, 1-212, and 65,-212 airfoils with 0.20 airfoil-chord split...
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