Merrill H. Mead
naca-rm-a51k05
Jan 1952
The variations with Mach number and angle of attack of the dynamic rolling-moment characteristics of a slender body of revolution in combination with a cruciform tail have been investigated in the Ames 6- by 6-foot supersonic wind tunnel.
An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1952/naca-rm-a51k05.pdf