| dc.creator |
Bradley, W. G. |
|
| dc.date |
2017-07-13T15:39:32Z |
|
| dc.date |
2017-07-13T15:39:32Z |
|
| dc.date |
1965-04 |
|
| dc.date.accessioned |
2020-11-30T18:29:57Z |
|
| dc.date.available |
2020-11-30T18:29:57Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/12191 |
|
| dc.identifier.uri |
http://dspace.lib.cranfield.ac.uk/handle/1826/12191 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4143 |
|
| 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. |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics |
|
| dc.relation |
CoA/N/AERO-165 |
|
| dc.relation |
165 |
|
| dc.title |
Measurement of the moments of inertia of a hawker siddeley dove Mk. 5 aircraft |
|
| dc.type |
Report |
|