A flight simulator investigation of the effect of turbulence on rolling requirements at low speed

dc.contributor.author	A. G. Barnes	en_US
dc.contributor.author	N. A. Parsons	en_US
dc.date.accessioned	2014-10-21T15:50:42Z
dc.date.available	2014-10-21T15:50:42Z
dc.date.issued	1970	en_US
dc.identifier.other	ARC/R&M-3697	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/2972
dc.description.abstract	This report describes a moving base simulator investigation of the rolling requirements in turbulence of an aircraft on the landing approach. A typical swept fighter type aircraft was simulated and pilot opinions were obtained for differing values of the maximum rolling acceleration for full aileron and for differing levels of turbulence. Known aircraft were also simulated for comparison with the results of the parametric study.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	A flight simulator investigation of the effect of turbulence on rolling requirements at low speed	en_US