| Download | - View final version: CFD study of sting effects (PDF, 2 MB)
|
|---|
| DOI | Resolve DOI: https://doi.org/10.4224/21276131 |
|---|
| Author | Search for: Kumar, Sanjiv1 |
|---|
| Name affiliation | - National Research Council of Canada. NRC Institute for Aerospace Research
|
|---|
| Format | Text, Technical Report |
|---|
| Physical description | 28 p. |
|---|
| 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. |
|---|
| Publication date | 1999-09 |
|---|
| Publisher | National Research Council of Canada. Institute for Aerospace Research |
|---|
| Series | |
|---|
| Language | English |
|---|
| NPARC number | 21276131 |
|---|
| Export citation | Export as RIS |
|---|
| Report a correction | Report a correction (opens in a new tab) |
|---|
| Record identifier | bd347d67-d43d-468e-a42c-e63550d807bc |
|---|
| Record created | 2015-09-25 |
|---|
| Record modified | 2022-11-07 |
|---|
