Analysis of damping derivatives for delta wings in hypersonic flow for curved leading edges with full sine wave
In this study, an attempt is made to evaluate the effect of first arched ends on the damping derived due to the pitch rate aimed at the variable sine wave bounty, flow deflection angle δ, pivot position, and the Mach numbers. Results show that with the escalation in the bounty of the complete sine w...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English English |
| Published: |
Blue Eyes Intelligence Engineering & Sciences Publication
2019
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/75893/ http://irep.iium.edu.my/75893/ http://irep.iium.edu.my/75893/ http://irep.iium.edu.my/75893/1/Renita-paper.pdf http://irep.iium.edu.my/75893/7/75893_Analysis%20of%20Damping%20Derivatives%20for%20Delta%20Wings_Scopus.pdf |