| dc.creator |
Radok, J. R. M. |
|
| dc.date |
2012-07-26T13:19:10Z |
|
| dc.date |
2012-07-26T13:19:10Z |
|
| dc.date |
1952-04 |
|
| dc.date.accessioned |
2022-05-09T10:17:19Z |
|
| dc.date.available |
2022-05-09T10:17:19Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/7432 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4732 |
|
| dc.description |
Using oblique coordinates, integro-differential equations of motion of aircraft with swept wings are deduced from Hamilton’s Principle for the dynamic problems of aero-elasticity, i.e. for the problems of free vibrations, flutter, dynamic stability and gust loads. |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield |
|
| dc.relation |
College Report |
|
| dc.relation |
58 |
|
| dc.title |
Dynamic aeroelasticity of aircraft with swept wings |
|
| dc.type |
Report |
|