Observations of the flow over a two-dimensional 4 per cent thick aerofoil at transonic speeds

dc.contributor.author	B. D. Henshall	en_US
dc.contributor.author	R. F. Cash	en_US
dc.date.accessioned	2014-10-21T15:55:00Z
dc.date.available	2014-10-21T15:55:00Z
dc.date.issued	1959	en_US
dc.identifier.other	ARC/R&M-3180	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3748
dc.description.abstract	Flow photographs and detailed pressure distributions for a 4 per cent thick circular-arc biconvex aerofoil at transonic speeds are presented. The results for incidences of 0, 1, 2 and 5 deg are analysed in detail.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Observations of the flow over a two-dimensional 4 per cent thick aerofoil at transonic speeds	en_US