| dc.creator |
Radok, J. R. M. |
|
| dc.date |
2012-07-25T14:27:42Z |
|
| dc.date |
2012-07-25T14:27:42Z |
|
| dc.date |
1952-03 |
|
| 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/1826/7420 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4730 |
|
| dc.description |
Using oblique coordinates, the static problems of Aero-elasticity for swept wings are reduced to the solution of integral – or matrix equations, which may be solved by iteration. The present treatment also indicates the suitability of integral equations for fundamental aero-elastic investigations. Continues … |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield |
|
| dc.relation |
College Report |
|
| dc.relation |
55 |
|
| dc.title |
Aileron reversal and divergence of swept wings with special consideration of the relevant aerodynamic and elastic characteristics |
|
| dc.type |
Report |
|