| 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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| Author | Search for: LaBerge, J. G.1; Search for: Boyer, D. W.1 |
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| Affiliation | - National Research Council of Canada
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| Format | Text, Memorandum |
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| Physical description | 38 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 | 1955-10-24 |
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| Publisher | National Research Council of Canada. National Aeronautical Establishment. Aerodynamics |
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| Series | |
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| Is identical to | |
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| Language | English |
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| Peer reviewed | No |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | 8298cd76-0f77-40ac-998f-e39b74eabe7c |
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| Record created | 2020-11-26 |
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| Record modified | 2025-03-07 |
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