Arrow 1 and 2. Flight tests required for stability and control and damper development

Download	View final version: Arrow 1 and 2. Flight tests required for stability and control and damper development (PDF, 13.1 MiB)
DOI	Resolve DOI: https://doi.org/10.4224/40002206
Creator	Search for: Ewart, D. D.; Search for: Carley, R. R.
Format	Text, Technical Report
Physical description	1 PDF/A (13 MB), 53 p.
Subject	Avro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor
Publication date	1959-01
Date distributed online	2021-06-07
Publisher	Avro Aircraft Limited (Canada). Engineering Division
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.
Note	Publisher is assumed to be "Avro Aircraft Limited (Canada). Engineering Division" by the National Research Council of Canada. Distributed online by the National Research Council of Canada
Language	English
Identifier	71/FAR/23 Issue 2
Export citation	Export as RIS
Collection	Avro Canada CF-105 Arrow
Record identifier	b63324ad-1de4-4977-b4e6-9d4d1835b463
Record created	2021-06-03
Record modified	2021-06-07