The airborne path during take-off for constant rate-of-pitch manoeuvres

dc.contributor.author	D. H. Perry	en_US
dc.date.accessioned	2014-10-20T11:05:29Z
dc.date.available	2014-10-20T11:05:29Z
dc.date.issued	1969	en_US
dc.identifier.other	ARC/CP-1042	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1055
dc.description.abstract	A method of estimating the airborne path during take-off is proposed, based on the assumption that the aircraft is rotated at a constant rate of pitch from the moment of lift-off to the point at which it attains a steady climb path. The justification for this assumption is discussed. A simplified analysis, using small perturbation equations of motion, has been developed for initial project studies. Examples of the method applied to a slender wing transport aircraft, and a lightly loaded STOL aircraft are given, and the factors affecting the value of rate of pitch used are discussed.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	The airborne path during take-off for constant rate-of-pitch manoeuvres	en_US