NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Rocket-Model Measurements of Zero-Lift Damping in Roll of the Bell MX-776 Missile at Mach Numbers from 0.6 to 1.56The 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,
Document ID
20050029431
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Bland, William N., Jr.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Purser, Paul E.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 22, 2013
Publication Date
December 31, 1953
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-SL54A13
Report Number: NACA-RM-SL54A13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available