A numerical solution for the equation of the lifting surface in subsonic flow including tunnel effects
We employ the images method to establish the lifting surface equation including tunnel effects. We obtain a 2d hypersingular integral and we utilize Gauss-type quadrature formulas to discretize it. Numerical calculations are performed for the elliptical and rectangular wings in order to calculate th...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2011-09-01
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| Series: | INCAS Bulletin |
| Subjects: | |
| Online Access: | http://bulletin.incas.ro/files/carabineanu_adrian_v3_is3_full.pdf |