A modification of the generalized airfoil equation and the corresponding numerical methods
The two-dimensional problem of steady, inviscid, irrotational, subsonic flow around a straight or curvilinear thin airfoil or an array of such airfoils inside a wind tunnel is generally reduced to a one-dimensional Cauchy type real or complex singular integral equation called generalized airfoil equ...
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Format: | Technical Report |
Language: | English |
Published: |
2018
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Online Access: | http://hdl.handle.net/10889/11214 |