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The forces and moments on airplane engine mounts (1936)
NASA Technical Reports Server (NTRS) · leaf 19
2.0 … Q -01 .02 .03 .04 .05 .16 nz/y tfigure 1.- Angular velocity of an airplane in pitch.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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