| dc.creator |
Hunter-Tod, J. H. |
|
| dc.date |
2012-05-15T14:35:32Z |
|
| dc.date |
2012-05-15T14:35:32Z |
|
| dc.date |
1949-03 |
|
| dc.date.accessioned |
2022-05-09T10:17:17Z |
|
| dc.date.available |
2022-05-09T10:17:17Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/7153 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4705 |
|
| dc.description |
Expressions are derives for the yawing derivatives on the assumptions of the linearised theory of flow for a delta wing with small dihedral flying at supersonic speeds at small incidences.
The non-dimensional derivatives are numerically decreasing functions of Mach number. The non-dimensional rolling and yawing derivatives are also numerically decreasing functions of aspect ratio.
When the wing lies entirely within the apex Mach cone there is a leading edge suction force proportional to incidence which makes a destabilising contribution to the yawing moment and side force which may be of the same magnitude as that from the inducted excess pressure distribution. |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield |
|
| dc.relation |
College Report |
|
| dc.relation |
28 |
|
| dc.title |
The aerodynamic derivatives with respect to rate of yaw for a delta wing with small dihedral at supersonic speeds |
|
| dc.type |
Report |
|