Busing, J. R.; Marson, G. B.; Lilley, G. M.
(College of Aeronautics, 1955-06)
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 ...