Free-flight investigation, including some effects of wing aeroelasticity, of the rolling effectiveness of an all-movable horizontal tail with differential incidence at Mach numbers from 0.6 to 1.5

English, Roland D
naca-rm-l54k30
January 25, 1955


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1955/naca-rm-l54k30.pdf