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 |
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| container_end_page | 760 |
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| container_issue | 12 |
| container_start_page | 758 |
| container_title | Journal of aircraft |
| container_volume | 10 |
| creator | Crews, S. T Hohenemser, K. H Ormiston, R. A |
| description | 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. |
| doi_str_mv | 10.2514/3.60302 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 0021-8669 |
| ispartof | Journal of aircraft, 1973-12, Vol.10 (12), p.758-760 |
| issn | 0021-8669 1533-3868 |
| language | eng |
| recordid | cdi_crossref_primary_10_2514_3_60302 |
| source | Alma/SFX Local Collection |
| title | An Unsteady Wake Model for a Hingeless Rotor |
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