Influence of compressor exit conditions on combustor annular diffusers. II - Flow redistribution
In gas-turbine engines the velocity of air, issuing from the compressor, must be reduced in order to permit effective operation of the downstream comhustor. This is partly achieved by locating an annular diffuser behind the compressor outlet guide vanes (OGVs); in modern systems, the inlet of this d...
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| Veröffentlicht in: | Journal of propulsion and power 2001-05, Vol.17 (3), p.687-694 |
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| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | eng |
| Online-Zugang: | Volltext |
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