Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow
In this paper the focus is on study of surface pressure distribution variation with angle of incidence and Mach number for hypersonic flow/Supersonic flow for a delta wing with leading edges which are curved. It is found that the surface pressure on the wing increases with increase in incidence ang...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English English |
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NOVA Science Publishers
2016
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| Online Access: | http://irep.iium.edu.my/53341/ http://irep.iium.edu.my/53341/1/paper2.pdf http://irep.iium.edu.my/53341/7/53341-Estimation%20of%20surface%20pressure%20distribution%20on%20a%20delta%20wing%20with%20curved%20leading%20edges_SCOPUS.pdf |
| _version_ | 1848784216923308032 |
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| author | Crasta, Asha Pavithra, S Khan, Sher Afghan |
| author_facet | Crasta, Asha Pavithra, S Khan, Sher Afghan |
| author_sort | Crasta, Asha |
| building | IIUM Repository |
| collection | Online Access |
| description | In this paper the focus is on study of surface pressure distribution variation with angle of incidence and Mach number for hypersonic flow/Supersonic flow for a delta
wing with leading edges which are curved. It is found that the surface pressure on the wing increases with increase in incidence angle and the inertia level. Results are compared for M = 8.7, 10, and 17 for delta wing with leading edge straight and curved and the results are found to be in good agreement with existing theories. |
| first_indexed | 2025-11-14T16:33:44Z |
| format | Article |
| id | iium-53341 |
| institution | International Islamic University Malaysia |
| institution_category | Local University |
| language | English English |
| last_indexed | 2025-11-14T16:33:44Z |
| publishDate | 2016 |
| publisher | NOVA Science Publishers |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | iium-533412017-03-15T02:15:02Z http://irep.iium.edu.my/53341/ Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow Crasta, Asha Pavithra, S Khan, Sher Afghan T175 Industrial research. Research and development In this paper the focus is on study of surface pressure distribution variation with angle of incidence and Mach number for hypersonic flow/Supersonic flow for a delta wing with leading edges which are curved. It is found that the surface pressure on the wing increases with increase in incidence angle and the inertia level. Results are compared for M = 8.7, 10, and 17 for delta wing with leading edge straight and curved and the results are found to be in good agreement with existing theories. NOVA Science Publishers 2016 Article PeerReviewed application/pdf en http://irep.iium.edu.my/53341/1/paper2.pdf application/pdf en http://irep.iium.edu.my/53341/7/53341-Estimation%20of%20surface%20pressure%20distribution%20on%20a%20delta%20wing%20with%20curved%20leading%20edges_SCOPUS.pdf Crasta, Asha and Pavithra, S and Khan, Sher Afghan (2016) Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow. International Journal of Energy, Environment, and Economics, 24 (1). pp. 67-73. ISSN 1054-853X http://www.novapublishers.com |
| spellingShingle | T175 Industrial research. Research and development Crasta, Asha Pavithra, S Khan, Sher Afghan Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow |
| title | Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow |
| title_full | Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow |
| title_fullStr | Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow |
| title_full_unstemmed | Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow |
| title_short | Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow |
| title_sort | estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow |
| topic | T175 Industrial research. Research and development |
| url | http://irep.iium.edu.my/53341/ http://irep.iium.edu.my/53341/ http://irep.iium.edu.my/53341/1/paper2.pdf http://irep.iium.edu.my/53341/7/53341-Estimation%20of%20surface%20pressure%20distribution%20on%20a%20delta%20wing%20with%20curved%20leading%20edges_SCOPUS.pdf |