The effect of combined boundary-layer suction and base bleed on the drag of a 10 degree cone at M = 2.58

dc.contributor.author	E. L. Goldsmith	en_US
dc.contributor.author	N. A. Evans	en_US
dc.contributor.author	G. V. F. Smith	en_US
dc.date.accessioned	2014-10-21T15:50:01Z
dc.date.available	2014-10-21T15:50:01Z
dc.date.issued	1967	en_US
dc.identifier.other	ARC/R&M-3591	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/2859
dc.description.abstract	It has been shown experimentally at M = 2.58 that by removing a small quantity of air from the boundary layer through fine slits in the surface of a cone the transition Reynolds number can be increased from its natural value of 2.5 x 10power6 to 9 x 10power6. The air sucked from the surface has been discharged into the cone base region and it has been shown that the measured axial force on the body at zero incidence has been reduced over the whole test Reynolds number range (2.5 - 14 x 10power6).	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The effect of combined boundary-layer suction and base bleed on the drag of a 10 degree cone at M = 2.58	en_US