Influence of fuselage and canard-type control surface on the flow field adjacent to a rearward fuselage station at a Mach number of 2.0 : data presentation

Leonard J. Obery, Evan A. Fradenburgh, John F. Mello
naca-rm-e51k05
Jan 1952

Measurements of the local total pressures and flow-deflection angles in the flow field of a body and a canard-type control-surface combination were made at a rearward fuselage station (69 percent of the body length downstream of the nose) which corresponded to a possible engine inlet location.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1952/naca-rm-e51k05.pdf