Numerical Methods for Aerodynamic Shape Optimization
Gradient-based aerodynamic shape optimization, based on Computational Fluid Dynamics analysis of the flow, is a method that can automatically improve designs of aircraft components. The prospect is to reduce a cost function that reflects aerodynamic performances. When the shape is described by a lar...
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| Format: | Doctoral Thesis |
| Language: | English |
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Uppsala universitet, Avdelningen för teknisk databehandling
2005
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-6252 http://nbn-resolving.de/urn:isbn:91-554-6431-9 |