Measurement of the moments of inertia of a hawker siddeley dove Mk. 5 aircraft
| dc.contributor.author | Bradley, W. G. | |
| dc.date.accessioned | 2017-07-13T15:39:32Z | |
| dc.date.available | 2017-07-13T15:39:32Z | |
| dc.date.issued | 1965-04 | |
| dc.description.abstract | This note describes the measurement of the moments of inertia in roll, pitch and yaw of a Hawker-Siddeley (de Havilland) Dove Mk. 5 aircraft, using a spring-restrained oscillation technique. Using the present equipment it did not prove possible to measure the product of inertia. Inertias mere measured in six different fuel conditions . The results are given in Tables I - V. A device was developed which measures the periods of oscillation of large structures, quicker and more accurately than hitherto possible. This device is described in the Appendix. | en_UK |
| dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/12191 | |
| dc.language.iso | en | en_UK |
| dc.publisher | College of Aeronautics | en_UK |
| dc.relation.ispartofseries | CoA/N/AERO-165 | en_UK |
| dc.relation.ispartofseries | 165 | en_UK |
| dc.title | Measurement of the moments of inertia of a hawker siddeley dove Mk. 5 aircraft | en_UK |
| dc.type | Report | en_UK |