Jack N. Nielsen, Elliott D. Katzen, Kenneth K. Tang
naca-rm-a50f06
Sep 1950
In order to investigate the effects of interference on wing-body combinations, tests were conducted at Mach numbers of 1.50 and 2.02 of a pointed, cylindrical body, of six triangular wings having aspect ratios from 0.67 to 4.00, and of the wings and the body in combination.
An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1950/naca-rm-a50f06.pdf