Low-speed wind-tunnel tests on a 1/8th scale model of the Handley-Page HP.115

dc.contributor.author	P. B. E. Engler	en_US
dc.contributor.author	G. F. Moss	en_US
dc.date.accessioned	2014-10-21T15:56:37Z
dc.date.available	2014-10-21T15:56:37Z
dc.date.issued	1965	en_US
dc.identifier.other	ARC/R&M-3486	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/4062
dc.description.abstract	A series of tunnel tests was made on a slender wing design to provide a basis for the flight-tunnel comparison of data and to give general wind-tunnel support for the flight research work on the aeroplane. The interim comparisons with flight which have been possible so far show good agreement as regards lift and lateral and directional stability, but significant differences in some control derivatives.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Low-speed wind-tunnel tests on a 1/8th scale model of the Handley-Page HP.115	en_US