A MODEL FOR AERODYNAMICAL DATA STRUCTURE; GRAPHICAL INTERFACE AND USER’S FACILITIES
This model defines the structure and applicability of aero dynamical complex data (up to four dimensions without flap influence which is separate considered) in steady states calculus for different configurations and optional cases (ground effect, asymmetrical propulsion (one of engines out) as well...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2010-03-01
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| Series: | INCAS Bulletin |
| Online Access: | http://bulletin.incas.ro/files/florentin_sperlea_v2no1_full.pdf |