Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings
In this study, an experimental and numerical investigation was carried out to obtain lift, drag, and pitching moment data on 65-deg delta and 65/40-deg double-delta wings. The experimental tests were conducted at the KFUPM low-speed wind tunnel facility whereas the numerical tests were performed usi...
محفوظ في:
| المؤلف الرئيسي: | |
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| مؤلفون آخرون: | , , |
| التنسيق: | article |
| منشور في: |
2008
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| الموضوعات: | |
| الوصول للمادة أونلاين: | https://eprints.kfupm.edu.sa/id/eprint/813/1/ja_20243_FSaeed_rev.pdf |
| الوسوم: |
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| _version_ | 1864513389205651456 |
|---|---|
| author | Al-Garni, Ahmed Z. |
| author2 | Saeed, Farooq Al-Garni, Abdullah M. unknown |
| author2_role | author author author |
| author_facet | Al-Garni, Ahmed Z. Saeed, Farooq Al-Garni, Abdullah M. unknown |
| author_role | author |
| dc.creator.none.fl_str_mv | Al-Garni, Ahmed Z. Saeed, Farooq Al-Garni, Abdullah M. unknown |
| dc.date.none.fl_str_mv | 2008-01-01 2020 |
| dc.format.none.fl_str_mv | application/pdf |
| dc.identifier.none.fl_str_mv | https://eprints.kfupm.edu.sa/id/eprint/813/1/ja_20243_FSaeed_rev.pdf (2008) Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings. AIAA Journal of Aircraft, 45 (1). pp. 71-76. |
| dc.language.none.fl_str_mv | en |
| dc.publisher.none.fl_str_mv | AIAA |
| dc.relation.none.fl_str_mv | https://eprints.kfupm.edu.sa/id/eprint/813/ http://www.aiaa.org |
| dc.rights.*.fl_str_mv | info:eu-repo/semantics/openAccess |
| dc.subject.none.fl_str_mv | Aerospace |
| dc.title.none.fl_str_mv | Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings |
| dc.type.none.fl_str_mv | Article PeerReviewed info:eu-repo/semantics/publishedVersion info:eu-repo/semantics/article |
| description | In this study, an experimental and numerical investigation was carried out to obtain lift, drag, and pitching moment data on 65-deg delta and 65/40-deg double-delta wings. The experimental tests were conducted at the KFUPM low-speed wind tunnel facility whereas the numerical tests were performed using the commercial CFD software FLUENT. Results from both experiments and numerical predictions were compared to other experimental data found in literature as well as to the theory of Polhamus. The results of comparison of surface pressure coefficient distribution and vortex breakdown location show good agreement with experiments. Overall the comparison of result shows good agreement between different experimental studies as well as good agreement with the CFD predictions and the theoretical calculations |
| eu_rights_str_mv | openAccess |
| format | article |
| id | KFUPM_dc0f26ed07959303f017ab8933dd7d1a |
| identifier_str_mv | (2008) Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings. AIAA Journal of Aircraft, 45 (1). pp. 71-76. |
| language_invalid_str_mv | en |
| network_acronym_str | KFUPM |
| network_name_str | King Fahd University of Petroleum and Minerals |
| oai_identifier_str | oai::813 |
| publishDate | 2008 |
| publisher.none.fl_str_mv | AIAA |
| repository.mail.fl_str_mv | |
| repository.name.fl_str_mv | |
| repository_id_str | |
| spelling | Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta WingsAl-Garni, Ahmed Z.Saeed, FarooqAl-Garni, Abdullah M.unknownAerospaceIn this study, an experimental and numerical investigation was carried out to obtain lift, drag, and pitching moment data on 65-deg delta and 65/40-deg double-delta wings. The experimental tests were conducted at the KFUPM low-speed wind tunnel facility whereas the numerical tests were performed using the commercial CFD software FLUENT. Results from both experiments and numerical predictions were compared to other experimental data found in literature as well as to the theory of Polhamus. The results of comparison of surface pressure coefficient distribution and vortex breakdown location show good agreement with experiments. Overall the comparison of result shows good agreement between different experimental studies as well as good agreement with the CFD predictions and the theoretical calculationsAIAA2008-01-012020ArticlePeerReviewedinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfhttps://eprints.kfupm.edu.sa/id/eprint/813/1/ja_20243_FSaeed_rev.pdf (2008) Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings. AIAA Journal of Aircraft, 45 (1). pp. 71-76. enhttps://eprints.kfupm.edu.sa/id/eprint/813/http://www.aiaa.orginfo:eu-repo/semantics/openAccessoai::8132019-11-01T13:25:22Z |
| spellingShingle | Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings Al-Garni, Ahmed Z. Aerospace |
| status_str | publishedVersion |
| title | Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings |
| title_full | Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings |
| title_fullStr | Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings |
| title_full_unstemmed | Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings |
| title_short | Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings |
| title_sort | Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings |
| topic | Aerospace |
| url | https://eprints.kfupm.edu.sa/id/eprint/813/1/ja_20243_FSaeed_rev.pdf |