Effect of Pulsed Film Cooling on Leading Edge Film Effectiveness
Detailed film effectiveness measurements have been made on a cylindrical leading edge surface for steady and pulsating flows. The film hole is off centered by 21.5 deg from the centerline and angled 20 deg to the surface and 90 deg from the streamwise direction. Two jet-to-cross-flow velocity ratios...
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Veröffentlicht in: | Journal of turbomachinery 2012-07, Vol.134 (4) |
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Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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