A wind-tunnel investigation of several wingless missile configurations at supersonic speeds

Reese, David E., Jr.
naca-rm-a57j22
1958


A wind-tunnel investigation of several wingless missile configurations was made. Lift, drag, and pitching-moment coefficients were measured on a series of models at Mach numbers of 2.44 and 3.35 and on one model from 1.76 to 5.05.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1958/naca-rm-a57j22.pdf