A flight investigation of the spinning of the NY-1 airplane with varied mass distribution and other modifications, and an analysis based on wind-tunnel tests (1934)
NASA Technical Reports Server (NTRS) · leaf 10
47 A FLIGHT INVESTIGATION OF THE SPINNING OF THE NT-l AIRPLANE … Angle of attack, degrees Fiquee 11.—Computed aerodynamlo and gyroscoplo rolling-moment coeffici- ti-84 ents, elevator ap 33°, ballast at e. j. i ^-82 o -Si t3° -78 10 20 30 40 50 60 70 80 Angle of attack, degrees Fiqube 14.—Equilibrium ol three moments, elevator up 33°, ballast at c t. -88 9 p-86 «…
NASA Technical Reports Server (NTRS)
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