Computation of stiffness derivative for an unsteady delta wing with curved leading edges
An attempt has been made to derive the expressions for stiffness derivative for a delta wing with curved leading edges for an unsteady high speed flow. It is evident from the figures that stiffness derivative decreases as Mach number increases. It is also seen that as amplitude of half sine wave i...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
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Institute of Institutional Industrial Research
2017
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/61843/ http://irep.iium.edu.my/61843/1/Paper-5-IJRRA-04-04-18.pdf |
| _version_ | 1848785747083001856 |
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| author | Monis, Renita Sharon Shabana, Ayesha Crasta, Asha Khan, Sher Afghan |
| author_facet | Monis, Renita Sharon Shabana, Ayesha Crasta, Asha Khan, Sher Afghan |
| author_sort | Monis, Renita Sharon |
| building | IIUM Repository |
| collection | Online Access |
| description | An attempt has been made to derive the expressions for stiffness derivative for a delta wing with curved leading
edges for an unsteady high speed flow. It is evident from the figures that stiffness derivative decreases as Mach number
increases. It is also seen that as amplitude of half sine wave increases the stiffness derivative also increases. This is an
improvement of previous theory as the effect of leeward surface are included in the present work. |
| first_indexed | 2025-11-14T16:58:03Z |
| format | Article |
| id | iium-61843 |
| institution | International Islamic University Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-14T16:58:03Z |
| publishDate | 2017 |
| publisher | Institute of Institutional Industrial Research |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | iium-618432018-02-05T07:43:41Z http://irep.iium.edu.my/61843/ Computation of stiffness derivative for an unsteady delta wing with curved leading edges Monis, Renita Sharon Shabana, Ayesha Crasta, Asha Khan, Sher Afghan QA297 Numerical Analysis An attempt has been made to derive the expressions for stiffness derivative for a delta wing with curved leading edges for an unsteady high speed flow. It is evident from the figures that stiffness derivative decreases as Mach number increases. It is also seen that as amplitude of half sine wave increases the stiffness derivative also increases. This is an improvement of previous theory as the effect of leeward surface are included in the present work. Institute of Institutional Industrial Research 2017-12 Article PeerReviewed application/pdf en http://irep.iium.edu.my/61843/1/Paper-5-IJRRA-04-04-18.pdf Monis, Renita Sharon and Shabana, Ayesha and Crasta, Asha and Khan, Sher Afghan (2017) Computation of stiffness derivative for an unsteady delta wing with curved leading edges. International Journal of Recent Research Aspects .., 4 (4). pp. 69-72. ISSN 2349-7688 https://www.ijrra.net/Vol4issue4/IJRRA-04-04-18.pdf |
| spellingShingle | QA297 Numerical Analysis Monis, Renita Sharon Shabana, Ayesha Crasta, Asha Khan, Sher Afghan Computation of stiffness derivative for an unsteady delta wing with curved leading edges |
| title | Computation of stiffness derivative for an unsteady delta wing with curved leading edges |
| title_full | Computation of stiffness derivative for an unsteady delta wing with curved leading edges |
| title_fullStr | Computation of stiffness derivative for an unsteady delta wing with curved leading edges |
| title_full_unstemmed | Computation of stiffness derivative for an unsteady delta wing with curved leading edges |
| title_short | Computation of stiffness derivative for an unsteady delta wing with curved leading edges |
| title_sort | computation of stiffness derivative for an unsteady delta wing with curved leading edges |
| topic | QA297 Numerical Analysis |
| url | http://irep.iium.edu.my/61843/ http://irep.iium.edu.my/61843/ http://irep.iium.edu.my/61843/1/Paper-5-IJRRA-04-04-18.pdf |