Low-speed model tests on two "V" wings

dc.contributor.author	J. Trouncer	en_US
dc.contributor.author	D. Kettle	en_US
dc.date.accessioned	2014-10-21T15:53:28Z
dc.date.available	2014-10-21T15:53:28Z
dc.date.issued	1947	en_US
dc.identifier.other	ARC/R&M-2364	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3466
dc.description.abstract	Wind tunnel tests were required for comparison with flight tests on two "V" wing tailless gliders of 28.4 deg. and 36.4 deg. sweepback. The main part of the work consisted of longitudinal, lateral and directional stability tests on the two wings, but pressure-plotting tests on the wing of larger sweepback and an investigation of anti-tip stalling devices was also included. Tip slats were found to be the most effective of the devices tried in the present experiments for overcoming the drawback of the premature tip stall.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Low-speed model tests on two "V" wings	en_US