Design optimisation of aeroengine compressor blades
Optimisation of multistage axial compressors is a time-demanding challenge in large need of effective methods. Traditionally, the design has been based on "trial-and-error" procedures, which count on the skills and experience of the designer to suggest redesigns that are likely to yield im...
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| Format: | Others |
| Language: | English |
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Luleå
2001
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-25824 |