| dc.creator |
Craven, A. H. |
|
| dc.date |
2014-09-25T15:04:36Z |
|
| dc.date |
2014-09-25T15:04:36Z |
|
| dc.date |
1960-01 |
|
| dc.date.accessioned |
2022-05-09T10:17:25Z |
|
| dc.date.available |
2022-05-09T10:17:25Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/8704 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4799 |
|
| dc.description |
Thin aerofoil theory is used to obtain, in integral form the
aerodynamic derivatives of an aerofoil oscillating in an infinite cascade.
The theory allows for arbitrary stagger angle and phase difference between
adjacent blades of the cascade. The expressions obtained reduce, for zero
stagger and for in phase and antiphase oscillations, to known results. |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics |
|
| dc.relation |
College of Aeronautics Report |
|
| dc.relation |
125 |
|
| dc.relation |
COA/125 |
|
| dc.title |
The aerodynamic derivatives of an aerofoil oscillating in an infinite staggered cascade |
|
| dc.type |
Report |
|