Numerical simulation of the flow about a swept wing with leading-edge ice accretions
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Kwon, Oh Joon | - |
| dc.contributor.author | Sankar, Lakshmi N. | - |
| dc.date.accessioned | 2008-02-20T02:19:25Z | - |
| dc.date.available | 2008-02-20T02:19:25Z | - |
| dc.date.issued | 1997-02 | - |
| dc.identifier.citation | Computers & Fluids, Volume 26, Issue 2, February 1997, Pages 183-192 | en |
| dc.identifier.issn | 0045-7930 | - |
| dc.identifier.uri | http://www.sciencedirect.com/science?_ob=ArticleURL&_udi=B6V26-3SMSN30-5&_user=170364&_rdoc=1&_fmt=&_orig=search&_sort=d&view=c&_acct=C000013318&_version=1&_urlVersion=0&_userid=170364&md5=f8646dd32c9cd7e4543dcd4ce1b295d2 | - |
| dc.identifier.uri | http://hdl.handle.net/10203/3079 | - |
| dc.description.abstract | The aerodynamic load characteristics and the performance degradation of moderate aspect ratio wings with simulated glaze leading-edge ice have been studied using a three-dimensional compressible Navier-Stokes solver. Correlation of predictions with experimental data for swept wings with and without leading-edge ice formation shows the ability of the present computational technique to predict accurately both the distributed surface pressures and integrated sectional loads. The leading-edge flow separation and reattachment on the wing surface caused by the leading-edge ice shape are also well captured, showing a vortex formation and the spanwise migration of the flow inside the separated flow region. The performance degradation of the wing as a result of the leading-edge ice formation is numerically well demonstrated. | en |
| dc.language.iso | en_US | en |
| dc.publisher | Elsevier | en |
| dc.subject | CFD | en |
| dc.subject | Swept wing | en |
| dc.title | Numerical simulation of the flow about a swept wing with leading-edge ice accretions | en |
| dc.type | Article | en |
| dc.identifier.doi | 10.1016/S0045-7930(96)00038-2 | - |
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- AE-Conference Papers(학술회의논문)
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