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...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English English |
| Published: |
NOVA Science Publishers
2016
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| Subjects: | |
| Online Access: | 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 http://irep.iium.edu.my/53341/ http://www.novapublishers.com |
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