Experimental investigation of the interference of a body on a low aspect ratio wing of rectangular planform at a Mach number of 2
| dc.contributor.author | Busing, J. R. | |
| dc.contributor.author | Marson, G. B. | |
| dc.contributor.author | Lilley, G. M. | |
| dc.date.accessioned | 2016-12-20T09:35:38Z | |
| dc.date.available | 2016-12-20T09:35:38Z | |
| dc.date.issued | 1955-06 | |
| dc.description.abstract | Results are given of pressure measurements on awing of gross aspect ratio approximately 2/3 mounted on a cylindrical body with an ogival nose, made at a Mach number of 2.00 in the 9in, x 9in, supersonic -wind tunnel at the College of Aeronautics. The wing section was a single wedge having a 6° total nose angle. The ranges of body incidence and roll in these tests were from 0° to 30°, and 0°, 30°, 600 and 90° respectively. The normal force, lift, drag and side force coefficients, and rolling and pitching moments were obtained from the pressure measurements. | en_UK |
| dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/11167 | |
| dc.language.iso | en | en_UK |
| dc.publisher | College of Aeronautics | en_UK |
| dc.relation.ispartofseries | CoA/N-31 | en_UK |
| dc.relation.ispartofseries | 31 | en_UK |
| dc.title | Experimental investigation of the interference of a body on a low aspect ratio wing of rectangular planform at a Mach number of 2 | en_UK |
| dc.type | Report | en_UK |