Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76

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...

وصف كامل

محفوظ في:
التفاصيل البيبلوغرافية
المؤلف الرئيسي: Al-Garni, Ahmed Z. (author)
مؤلفون آخرون: Saeed, F. (author), Al-Garni, A. M. (author), unknown (author)
التنسيق: article
منشور في: 2020
الموضوعات:
الوصول للمادة أونلاين:https://eprints.kfupm.edu.sa/id/eprint/290/1/2008-JA-Garni-delta.pdf
الوسوم: إضافة وسم
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
_version_ 1864513388499959808
author Al-Garni, Ahmed Z.
author2 Saeed, F.
Al-Garni, A. M.
unknown
author2_role author
author
author
author_facet Al-Garni, Ahmed Z.
Saeed, F.
Al-Garni, A. M.
unknown
author_role author
dc.creator.none.fl_str_mv Al-Garni, Ahmed Z.
Saeed, F.
Al-Garni, A. M.
unknown
dc.date.*.fl_str_mv 2020
dc.format.none.fl_str_mv application/pdf
dc.identifier.none.fl_str_mv https://eprints.kfupm.edu.sa/id/eprint/290/1/2008-JA-Garni-delta.pdf
Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76. AIAA Journal.
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/290/
dc.rights.*.fl_str_mv info:eu-repo/semantics/openAccess
dc.subject.none.fl_str_mv Aerospace
dc.title.none.fl_str_mv Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76
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_fbe91212b04f1c154fb7bc90b00734f1
identifier_str_mv Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76. AIAA Journal.
language_invalid_str_mv en
network_acronym_str KFUPM
network_name_str King Fahd University of Petroleum and Minerals
oai_identifier_str oai::290
publishDate 2020
publisher.none.fl_str_mv AIAA
repository.mail.fl_str_mv
repository.name.fl_str_mv
repository_id_str
spelling Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76Al-Garni, Ahmed Z.Saeed, F.Al-Garni, A. 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 calculations.AIAAArticlePeerReviewedinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfhttps://eprints.kfupm.edu.sa/id/eprint/290/1/2008-JA-Garni-delta.pdf Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76. AIAA Journal. enhttps://eprints.kfupm.edu.sa/id/eprint/290/2020info:eu-repo/semantics/openAccessoai::2902020-12-31T06:02:37Z
spellingShingle Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76
Al-Garni, Ahmed Z.
Aerospace
status_str publishedVersion
title Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76
title_full Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76
title_fullStr Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76
title_full_unstemmed Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76
title_short Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76
title_sort Al-Garni, A. Z., Saeed, F., Al-Garni, A. M., “Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings,” AIAA Journal of Aircraft, Vol. 45, No. 1, Jan.-Feb. 2008, pp. 71-76
topic Aerospace
url https://eprints.kfupm.edu.sa/id/eprint/290/1/2008-JA-Garni-delta.pdf