The aerodynamic derivatives with respect to rate of yaw for a delta wing with small dihedral at supersonic speeds
| dc.contributor.author | Hunter-Tod, J. H. | |
| dc.date.accessioned | 2012-05-15T14:35:32Z | |
| dc.date.available | 2012-05-15T14:35:32Z | |
| dc.date.issued | 1949-03 | |
| dc.description.abstract | 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. | en_UK |
| dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/7153 | |
| dc.language.iso | en | en_UK |
| dc.publisher | College of Aeronautics, Cranfield | en_UK |
| dc.relation.ispartofseries | College Report | en_UK |
| dc.relation.ispartofseries | 28 | en_UK |
| dc.title | The aerodynamic derivatives with respect to rate of yaw for a delta wing with small dihedral at supersonic speeds | en_UK |
| dc.type | Report | en_UK |