Experimental investigation of the stability, control, and induced rolling moments of a canard missile airframe at a Mach number of 1.7

Chubb, Robert S
naca-rm-a52g29
September 23, 1952

No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1952/naca-rm-a52g29.pdf