A general treatment of static longitudinal stability with propellers, with application to single-engined aircraft

dc.contributor.author	E. Priestley	en_US
dc.date.accessioned	2014-10-21T15:52:34Z
dc.date.available	2014-10-21T15:52:34Z
dc.date.issued	1944	en_US
dc.identifier.other	ARC/R&M-2732	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3280
dc.description.abstract	A general method of treatment of stick-fixed static longitudinal stability with propellers is given, distortion and compressibility effects being neglected. Model full-throttle data on some single-engined fighters are analysed for the flaps-up condition to establish a basis of estimation of effect of propeller on stability for this type of design. The general effect of propellers on manceuvre point, more particularly the effect on Hm - Kn, is considered in an appendix.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	A general treatment of static longitudinal stability with propellers, with application to single-engined aircraft	en_US