Download | - View final version: Minimum drag tests on the C-105 1/80 scale model (PDF, 2.0 MiB)
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DOI | Resolve DOI: https://doi.org/10.4224/40001824 |
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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 (1 MB), 7 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 | Zero lift drag measurements of a 1/80 scale model of the C-105 aircraft were made in the 30-inch tunnel at subsonic and supersonic speeds. The Mach number range extended from 0.53 to 1.57 corresponding to a Reynolds number range of 1.2 to 1.7 x 10⁶ based on wing mean aerodynamic chord, see Fig. 1. |
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Publication date | 1955 |
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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 | ac04d8dc-1d84-426f-b866-62e5a5435bd8 |
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Record created | 2021-06-03 |
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Record modified | 2022-05-19 |
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