| Alternative title | Supersonic wind tunnel tests on the effects of engine-off operation on lateral characteristics of the C-105 aircraft |
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| Download | - View final version: Supersonic tunnel tests on effects of engine-off operation on lateral characteristics of the C-105 aircraft (PDF, 14.3 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40001797 |
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| Creator | Search for: Laberge, J. G.; Search for: Boyer, D. W. |
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| Format | Text, Technical Report |
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| Physical description | 1 PDF/A (14 MB), 56 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 | The effect of blocking completely or partially one engine intake on the side force and yawing moment of the C-105 aircraft was investigated at supersonic speeds. A 1/80 scale model was tested in the 10 inch tunnel, the force and moment measurements being taken at a Mach number of 2.04. Schlieren photographs are presented for Mach numbers of 1.64 and 2.04.
Over the whole range of yaw angles explored complete blockage of one intake resulted in a yawing moment (ΔCₙ =0.001) tending to put the blocked intake on the windward side of the fuselage. |
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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 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 | e590bae4-a30b-40e4-bb55-d4c46420b812 |
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| Record created | 2021-06-03 |
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| Record modified | 2025-11-21 |
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