Aerodynamics investigation of delta wing at low Reynold’s number
A numerical simulation has been carried out to investigate the aerodynamics of an oscillating delta wing and to evaluate the flow structure over the leading edge at different low Reynolds numbers. The numerical results of the coefficient of lift (CL) vs angle of attack are validated with the experi...
| Main Authors: | , |
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| Format: | Article |
| Language: | English English |
| Published: |
Penerbit Akademia Baru
2019
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/70862/ http://irep.iium.edu.my/70862/ http://irep.iium.edu.my/70862/1/70862_Aerodynamics%20Investigation%20of%20Delta%20Wing.pdf http://irep.iium.edu.my/70862/7/70862_Aerodynamics%20investigation%20of%20delta%20wing_SCOPUS.pdf |