C105. Lateral stiffness of fuselage formers and adjacent wing structure. STN. 644·43, 697·28, 742·50, 538·77, 485·00

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DOI	Resolve DOI: https://doi.org/10.4224/40002497
Format	Text, Technical Report
Physical description	1 PDF/A (36 MB), 113 p.
Subject	Avro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor; design and construction
Publication date	1956-01-25
Date distributed online	2021-06-07
Publisher	Avro Aircraft Limited (Canada). Technical Department
Licence	Open Government Licence - Canada https://open.canada.ca/en/open-government-licence-canada
Access condition	The print copies are housed in the Rare books collection at the National Research Council of Canada. For access to print, permission to reproduce for commercial purposes, or questions related to the collection please contact NRC.NSL-BSN.CNRC@nrc-cnrc.gc.ca.
Series	Stress Report (Avro Aircraft Limited (Canada)), no. 7-0558-62.
Note	Author names are not decipherable. Distributed online by the National Research Council of Canada
Language	English
Export citation	Export as RIS
Collection	Avro Canada CF-105 Arrow
Record identifier	8d6316e0-0c89-4b4c-88f8-20dc3f32b825
Record created	2021-06-03
Record modified	2021-06-07

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