| Download | - View final version: Some zero-lift characteristics of a 1/80 scale model of the CF-105 aircraft at test Mach number of 1.57 (PDF, 3.2 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40001713 |
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| Creator | Search for: Laberge, J. G. |
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| Format | Text, Technical Report |
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| Physical description | 1 PDF/A (3 MB), 10 p. |
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| Subject | Avro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor |
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| Abstract | At supersonic speeds the values of C ₘₒ predicted and measured by the N.A.E. were found to disagree with the values measured by the N.A.C.A. In an attempt to discover a possible explanation for this discrepancy a detailed investigation was made in the area of interest and at a Mach number of 1.57. The effect of tunnel flow angularity was assessed by testing the model in both the inverted and upright positons while the effect of flow through the rather long and narrow intake ducts of the model was determined by testing the model with and without fairings over the intakes. In addition the effect of duct flow on the drag was determined at zero lift. |
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| Publication date | 1957 |
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| Date distributed online | 2021-06-07 |
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| Publisher | National Research Council of Canada. National Aeronautical Establishment. Aerodynamics |
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| Licence | |
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| 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.
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| Series | |
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| Note | Distributed online by the National Research Council of Canada |
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| Language | English |
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| Export citation | Export as RIS |
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| Collection | Avro Canada CF-105 Arrow |
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| Record identifier | d67318d5-1670-481d-a049-0b5fabe301e1 |
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| Record created | 2021-06-03 |
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| Record modified | 2022-05-19 |
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