Aerodynamics of porous airfoils and wings
This paper presents novel wind tunnel test results on the aerodynamics of a symmetric thin porous airfoil and a porous rectangular half wing using a symmetric thin airfoil as its cross section, obtained by a six-component force balance. The variation of lift coefficient, drag coefficient, pitching...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English English English |
| Published: |
SpringerLink
2018
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/64676/ http://irep.iium.edu.my/64676/ http://irep.iium.edu.my/64676/ http://irep.iium.edu.my/64676/1/Aerodynamics%20of%20permeable%20airfoils%20and%20wings-published.pdf http://irep.iium.edu.my/64676/7/64676_Aerodynamics%20of%20porous%20airfoils%20and%20wings_SCOPUS.pdf http://irep.iium.edu.my/64676/13/64676_Aerodynamics%20of%20porous%20airfoils%20and%20wings_WOS.pdf |