C105. Control surface limitations due to max. available high moments, and sideslip limitation due to maximum permissible fin load

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DOIResolve DOI: https://doi.org/10.4224/40002232
CreatorSearch for: Foster, D. J.; Search for: Garland, D.
FormatText, Technical Report
Physical description1 PDF/A (2 MB), 8 p.
SubjectAvro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor
Publication date
Date distributed online2021-06-07
PublisherAvro Aircraft Limited (Canada). Technical Department
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  • 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.
NoteDistributed online by the National Research Council of Canada
LanguageEnglish
IdentifierP/Control/97
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CollectionAvro Canada CF-105 Arrow
Record identifier88bf85d9-108c-49ee-9a68-4354192270ec
Record created2021-06-03
Record modified2021-06-07
Date modified: