An Unsteady Wake Model for a Hingeless Rotor
A simple nonsteady wake model derived from the unsteady moment of the momentum equation for zero advance ratio is correlated with cyclic pitch frequency response tests conducted with a small hingeless rotor model. Two and three or more bladed rotor analyses are presented.
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| Veröffentlicht in: | Journal of aircraft 1973-12, Vol.10 (12), p.758-760 |
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| Hauptverfasser: | , , |
| Format: | Artikel |
| Sprache: | eng |
| Online-Zugang: | Volltext |
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| Zusammenfassung: | A simple nonsteady wake model derived from the unsteady moment of the momentum equation for zero advance ratio is correlated with cyclic pitch frequency response tests conducted with a small hingeless rotor model. Two and three or more bladed rotor analyses are presented. |
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| ISSN: | 0021-8669 1533-3868 |
| DOI: | 10.2514/3.60302 |