Experimental investigation of counter-rotating propfan flutter at cruise conditions
This article presents wind-tunnel experimental flutter results, at transonic relative flows, for a 0.62-m-diam composite propfan model. A blade row that fluttered was tested alone and with a stable aft counter-rotating blade row. The major objectives of the experiment were to study the effects of th...
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| Veröffentlicht in: | Journal of propulsion and power 1994-05, Vol.10 (3), p.343-347 |
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| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
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