Critical Reversal Speed
THIS article is intended, firstly, as a means to a quick approximate determination of the critical reversal speed of a wing, and secondly to give a clearer insight of why approximations can be given for the general formula for determining K, when the aileron chord and wing chord are of linear taper...
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| Veröffentlicht in: | Aircraft Engineering and Aerospace Technology 1943-11, Vol.15 (11), p.319-324 |
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| Sprache: | eng |
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| container_end_page | 324 |
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| container_issue | 11 |
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| container_title | Aircraft Engineering and Aerospace Technology |
| container_volume | 15 |
| creator | Horton, W.H |
| description | THIS article is intended, firstly, as a means to a quick approximate determination of the critical reversal speed of a wing, and secondly to give a clearer insight of why approximations can be given for the general formula for determining K, when the aileron chord and wing chord are of linear taper at least over the aileron portion. |
| doi_str_mv | 10.1108/eb031070 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 0002-2667 |
| ispartof | Aircraft Engineering and Aerospace Technology, 1943-11, Vol.15 (11), p.319-324 |
| issn | 0002-2667 |
| language | eng |
| recordid | cdi_emerald_primary_10_1108_eb031070 |
| source | Emerald Journals |
| title | Critical Reversal Speed |
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