Evaluation of stiffness derivative for a delta wing with straight leading edges in unsteady flow
The emphasis of this paper is to examine the Stiffness derivative variation with the pivot position by varying Mach number in unsteady flow and its comparison with quasi-steady the flow of Crasta& Khan for varying angle of attack with different Mach number. From the results, it is evident that...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English English |
| Published: |
Blue Eyes Intelligence Engineering & Sciences
2019
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/72843/1/Renita.pdf http://irep.iium.edu.my/72843/7/72843_Evaluation%20of%20stiffness%20derivative%20for%20a%20delta%20wing%20with%20straight%20leading%20edges%20in%20unsteady%20flow_Scopus.pdf http://irep.iium.edu.my/72843/ https://www.ijeat.org/wp-content/uploads/papers/v8i3S/C11610283S19.pdf |
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http://irep.iium.edu.my/72843/1/Renita.pdfhttp://irep.iium.edu.my/72843/7/72843_Evaluation%20of%20stiffness%20derivative%20for%20a%20delta%20wing%20with%20straight%20leading%20edges%20in%20unsteady%20flow_Scopus.pdf
http://irep.iium.edu.my/72843/
https://www.ijeat.org/wp-content/uploads/papers/v8i3S/C11610283S19.pdf