Flight investigation of the effects of horizontal-tail height, moment of inertia, and control effectiveness on the pitch-up characteristics of a 35 degree swept-wing fighter airplane at high subsonic speeds

Mcfadden, Norman M Heinle, Donovan R
naca-rm-a54f21
January 18, 1954


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1954/naca-rm-a54f21.pdf