Measurement of the derivative zw for oscillating wings in cascade
| dc.contributor.author | Milne, R. D. | |
| dc.date.accessioned | 2013-03-12T12:17:45Z | |
| dc.date.available | 2013-03-12T12:17:45Z | |
| dc.date.issued | 1955-07 | |
| dc.description.abstract | Experimental results are reported of the damping derivative zw. for rigid rectangular wings of various aspect ratios in cascades having gap-chord ratios of 2, 1,1/2, 1/3, 1/4. The results show fair agreement with two-dimensional theory. The ranges of Reynolds numbers and frequency parameters were 0.8 to 2.5 x 10) and 0.1 to 0.45 respectively. The results show a strong dependence on Reynolds number which increases with decrease in gap-chord ratio. This effect was eliminated by transition fixation by wires placed at suitable positions down-stream of the wing leading edge. | en_UK |
| dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/7853 | |
| dc.language.iso | en | en_UK |
| dc.publisher | College of Aeronautics, Cranfield. | en_UK |
| dc.relation.ispartofseries | College Report | en_UK |
| dc.relation.ispartofseries | 93 | en_UK |
| dc.title | Measurement of the derivative zw for oscillating wings in cascade | en_UK |
| dc.type | Report | en_UK |