The effect of slipstream on the longitudinal stability of multi-engined aircraft

dc.contributor.author	D. E. Morris	en_US
dc.contributor.author	J. C. Morrall	en_US
dc.date.accessioned	2014-10-21T15:52:23Z
dc.date.available	2014-10-21T15:52:23Z
dc.date.issued	1948	en_US
dc.identifier.other	ARC/R&M-2701	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3247
dc.description.abstract	Flight measurements of longitudinal stability power-off and power-on made on numerous aircraft have been analysed and a generalised curve for estimating the contribution of slipstream to longitudinal stability, applicable to both flaps-up and flaps-down cases, has been derived. Using this curve the change in stability due to slipstream at a given value of CL can be estimated with a probable error of less than ± 0.02 in the position of the neutral point.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The effect of slipstream on the longitudinal stability of multi-engined aircraft	en_US