| dc.contributor.author | J. S. Thompson | en_US | 
| dc.contributor.author | R. A. Fail | en_US | 
| dc.contributor.author | J. V. Inglesby | en_US | 
| dc.date.accessioned | 2014-10-20T11:05:37Z | |
| dc.date.available | 2014-10-20T11:05:37Z | |
| dc.date.issued | 1969 | en_US | 
| dc.identifier.other | ARC/CP-1097 | en_US | 
| dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/1110 | |
| dc.description.abstract | Low-speed tunnel tests on a model of the HP 115 aircraft have provided a complete set of lateral derivatives for a range of frequency parameters. Over a range appropriate to full scale flight, the effects of frequency parameter are small, but for very high values there is a marked reduction in the derivatives ... Some information is included on the derivatives ... and there is evidence that the virtual inertias are about the same wind-on and wind-off. The Paper also describes some recent improvements in technique. | en_US | 
| dc.relation.ispartofseries | Aeronautical Research Council Current Papers | en_US | 
| dc.title | Low-speed wind-tunnel measurements of the oscillatory lateral stability derivatives for a model of a slender aircraft (HP 115) including the effects of frequency parameter | en_US |