An analysis of some major factors involved in normal take-off performance

dc.contributor.author	D. H. Perry	en_US
dc.date.accessioned	2014-10-20T11:05:27Z
dc.date.available	2014-10-20T11:05:27Z
dc.date.issued	1967	en_US
dc.identifier.other	ARC/CP-1034	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1047
dc.description.abstract	An analytical study has been made of the effect of such parameters as wing loading, aspect ratio, thrust-weight ratio, and number of engines, on the takeoff performance of fixed wing aircraft. Expressions are derived for the take-off lift coefficients which give the shortest take-off distance, the highest takeoff wing loading, and climb conditions just meeting the airworthiness requirements. Examples of the analysis applied to two designs of current interest are given.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	An analysis of some major factors involved in normal take-off performance	en_US