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Data obtained during low speed wind tunnel tests of 0.07 scale C-105 model (wing no. 1)

From National Research Council Canada

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DOIResolve DOI: https://doi.org/10.4224/40001820
CreatorSearch for: Pocock, P. J.
FormatText, Technical Report
Physical description1 PDF/A (1 MB), 22 p.
SubjectAvro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor
Abstract
The major portion of the available testing time during the first C-105 test programme was devoted to modification of the strut supports and strut-model attachment details. Also the elevator hinge was modified as the elevator slipped considerably during the first test runs. In view of the time consumed by the above activities it was not possible to complete very many test runs. It was possible to complete one run plus the five correction runs required. The present note is intended simply as a record of the test results that were obtained in the above force tests as well as in some flow visualization tests. The results of all the correction runs have been included.
Publication date
Date distributed online2021-06-07
PublisherNational Research Council of Canada. National Aeronautical Establishment. Aerodynamics
Licence
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
  • Laboratory Memorandum (National Research Council of Canada. National Aeronautical Establishment), no. AE-46c.
NoteDistributed online by the National Research Council of Canada
LanguageEnglish
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CollectionAvro Canada CF-105 Arrow
Record identifier9bb41f4c-eff3-4c9a-a503-aa22e5e8b60e
Record created2021-06-03
Record modified2022-05-19
Date modified: