| Download | - View final version: CFD study of sting effects (PDF, 2.4 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/21276131 |
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| Author | Search for: Kumar, Sanjiv1 |
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| Affiliation | - National Research Council Canada. NRC Institute for Aerospace Research
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| Format | Text, Technical Report |
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| Physical description | 28 p. |
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| Abstract | A CFD study has been carried out to assess the sting mounting effect for the 1/16th scale model of the aurora aircraft. Two sting geometries at three angles of attack are studies. These studies indicate that sting geometry close to the fuselage does have a significant effect on the pressure distribution and that this effect is largely attributable to blockage caused by the sting. |
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| Publication date | 1999-09 |
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| Publisher | National Research Council of Canada. Institute for Aerospace Research |
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| Series | |
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| Language | English |
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| NPARC number | 21276131 |
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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 | bd347d67-d43d-468e-a42c-e63550d807bc |
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| Record created | 2015-09-25 |
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| Record modified | 2022-11-07 |
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