Static stability of a compound wing configuration in ground effect
The height static stability of a wing can be a main concern for conceptual design of wing-in-ground effect (WIG) crafts. In this research, the stability of a rectangular and compound wing was computationally predicted in ground effect. A realizable k-e turbulent model was used for simulation the flo...
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Online Access: | http://eprints.utm.my/id/eprint/62659/1/AdiMaimun2014_StaticStabilityofaCompoundWing.pdf http://eprints.utm.my/id/eprint/62659/ http://dx.doi.org/10.11113/jt.v69.3282 |
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my.utm.626592017-11-01T04:17:09Z http://eprints.utm.my/id/eprint/62659/ Static stability of a compound wing configuration in ground effect Jameia, Saeed Abdul Malik, Adi Maimun Tofa, M. Mobassher Nor Azwadi, Nor Azwadi Mansor, Shuhaimi Priyanto, Agoes TJ Mechanical engineering and machinery The height static stability of a wing can be a main concern for conceptual design of wing-in-ground effect (WIG) crafts. In this research, the stability of a rectangular and compound wing was computationally predicted in ground effect. A realizable k-e turbulent model was used for simulation the flow filed over the wing surfaces. First, the drag coefficient and lift to drag ratio of numerical simulation were validated by experimental data of the rectangular wing. Next, the stability of the compound wing respect to different ground clearances will be determined and compared with rectangular wing. This study illustrated a deep understanding of static stability of present compound wing in ground effect, which eventually can be a guideline for researchers and designers of WIG craft. Penerbit UTM Press 2014 Article PeerReviewed application/pdf en http://eprints.utm.my/id/eprint/62659/1/AdiMaimun2014_StaticStabilityofaCompoundWing.pdf Jameia, Saeed and Abdul Malik, Adi Maimun and Tofa, M. Mobassher and Nor Azwadi, Nor Azwadi and Mansor, Shuhaimi and Priyanto, Agoes (2014) Static stability of a compound wing configuration in ground effect. Jurnal Teknologi (Sciences and Engineering), 69 (7). pp. 159-162. ISSN 0127-9696 http://dx.doi.org/10.11113/jt.v69.3282 DOI:10.11113/jt.v69.3282 |
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TJ Mechanical engineering and machinery Jameia, Saeed Abdul Malik, Adi Maimun Tofa, M. Mobassher Nor Azwadi, Nor Azwadi Mansor, Shuhaimi Priyanto, Agoes Static stability of a compound wing configuration in ground effect |
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The height static stability of a wing can be a main concern for conceptual design of wing-in-ground effect (WIG) crafts. In this research, the stability of a rectangular and compound wing was computationally predicted in ground effect. A realizable k-e turbulent model was used for simulation the flow filed over the wing surfaces. First, the drag coefficient and lift to drag ratio of numerical simulation were validated by experimental data of the rectangular wing. Next, the stability of the compound wing respect to different ground clearances will be determined and compared with rectangular wing. This study illustrated a deep understanding of static stability of present compound wing in ground effect, which eventually can be a guideline for researchers and designers of WIG craft. |
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Article |
author |
Jameia, Saeed Abdul Malik, Adi Maimun Tofa, M. Mobassher Nor Azwadi, Nor Azwadi Mansor, Shuhaimi Priyanto, Agoes |
author_facet |
Jameia, Saeed Abdul Malik, Adi Maimun Tofa, M. Mobassher Nor Azwadi, Nor Azwadi Mansor, Shuhaimi Priyanto, Agoes |
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Jameia, Saeed |
title |
Static stability of a compound wing configuration in ground effect |
title_short |
Static stability of a compound wing configuration in ground effect |
title_full |
Static stability of a compound wing configuration in ground effect |
title_fullStr |
Static stability of a compound wing configuration in ground effect |
title_full_unstemmed |
Static stability of a compound wing configuration in ground effect |
title_sort |
static stability of a compound wing configuration in ground effect |
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Penerbit UTM Press |
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2014 |
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http://eprints.utm.my/id/eprint/62659/1/AdiMaimun2014_StaticStabilityofaCompoundWing.pdf http://eprints.utm.my/id/eprint/62659/ http://dx.doi.org/10.11113/jt.v69.3282 |
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