Numerical study of effect of spoiler configuration on wake vortex alleviation
A numerical investigation was undertaken to evaluate the capabilities of differential spoiler setting (DSS) in modifying the span-wise wing load and reducing hazard of wake vortices imposed on a following aircraft. Numerical simulations were carried out on a scaled, half-model aircraft under high l...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English English |
| Published: |
American Society of Civil Engineers
2015
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/44185/ http://irep.iium.edu.my/44185/ http://irep.iium.edu.my/44185/ http://irep.iium.edu.my/44185/1/ASENG-633_p1.pdf http://irep.iium.edu.my/44185/2/Hani-_ASCE_J_Aero-May_2015.docx |