Investigation of Load and Pressure Distribution on Wing with Wake Rollup for Low Speed Aircraft
The presented work shows a preliminary analytic method for estimation of load and pressure distributions on low speed wings with flow separation and wake rollup phenomena’s. A higher order vortex panel method is coupled with the numerical lifting line theory by means of iterative procedure includin...
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| Format: | article |
| Langue: | EN |
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Al-Khwarizmi College of Engineering – University of Baghdad
2018
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| Accès en ligne: | https://doaj.org/article/bc553febfc9049f58e61a9f6b61b463e |
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