Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow
In this paper attention is focussed on study of effect of Aspect ratio of the wing on roll moment derivatives at various angle of attack and Mach number for a Supersonic flow. It is been observed that there is a linear increment in rolling moment derivative with aspect ratio as well as with Angle...
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| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
IRA Publications
2016
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/50991/3/Asha_Crasta_-IJAER.pdf http://irep.iium.edu.my/50991/ http://www.ijaer.com/images/short_pdf/1465412616_Asha_Crasta_2.pdf |
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