dc.contributor.author | I. W. Kaynes | en_US |
dc.date.accessioned | 2014-10-21T15:50:35Z | |
dc.date.available | 2014-10-21T15:50:35Z | |
dc.date.issued | 1970 | en_US |
dc.identifier.other | ARC/R&M-3665 | en_US |
dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/2937 | |
dc.description.abstract | The energy spectrum of atmospheric turbulence is used to predict the normal acceleration response of a rigid aircraft. Particular reference is made to spanwise variations of gust velocity and this effect is described in terms of a general input spectrum which is applicable to any wing with a particular spanwise loading distribution operating under a wide range of conditions. Tables of the gust response factor and the number of zero crossings are presented for a range of parameters. | en_US |
dc.relation.ispartofseries | Aeronautical Research Council Reports & Memoranda | en_US |
dc.title | Aircraft Centre of Gravity Response to Two-Dimensional Spectra of Turbulence | en_US |