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DAMPING MEASUREMENTS WITH A STING-SUPPORTED BEARING-PIVOT DYNAMIC BALANCE
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AIR FORCE STATION TENN
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Results of damping-in-pitch tests of a flaredafterbody re-entry shape are presented. Measurements using a sting-supported bearing-pivot system were made at free-stream Mach number equals 8 and over an amplitude range up to about 11 deg. Author
APPROVED FOR PUBLIC RELEASE