Publication Date:
2019-07-11
Description:
The zero-lift damping in roll of the Bell MX-776 missile has been measured by a sting-mounted rocket-model technique at Mach numbers from 0.6 to 1.56. The damping-in-roll data, in general, show no unusual variation with Mach number. Aileron rolling-moment effectiveness derived from these data and previously obtained rolling-effectiveness data appear reasonable,
Keywords:
Aerodynamics
Type:
NACA-RM-SL54A13
Format:
application/pdf