| dc.creator |
Milne, R. D. |
|
| dc.date |
2013-03-12T11:48:45Z |
|
| dc.date |
2013-03-12T11:48:45Z |
|
| dc.date |
1955-07 |
|
| dc.date.accessioned |
2022-05-09T10:17:21Z |
|
| dc.date.available |
2022-05-09T10:17:21Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/7852 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4757 |
|
| dc.description |
A method is presented whereby the 'Slender Body Theory' can be applied to the determination of the unsteady aerodynamic forces acting on slender wings and wing-body combinations experiencing harmonic deformations in a compressible flow. The analysis holds for subsonic and supersonic speeds, subject to restrictions which are stated and discussed. |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield. |
|
| dc.relation |
College Report |
|
| dc.relation |
94 |
|
| dc.title |
The unsteady aerodynamic forces on deforming, low aspect ratio wings and slender wing-body combinations oscillating harmonically in a compressible flow |
|
| dc.type |
Report |
|