Analysis for a wing nacelle configuration
The paper presents CFD results for a wing-nacelle configuration, in order to be testedagainst an analytic solution considering nacelles as chord discontinuities.
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2010-06-01
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| Series: | INCAS Bulletin |
| Subjects: | |
| Online Access: | http://bulletin.incas.ro/files/marwan_isper_v2no2_full.pdf |