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 11
f linear acceleration, each of the three moments, are given in Figure 14. referred to the center-of-gravity position of the original computations, should be included with the gyroscopic The curves of Figure 15 were obtained by a similar computation based on the model test with elevator moments. A… … charts would represent the conditions for a steady Angle of attack, degrees spin. Figuee 17.—Computed aerodynamlo and gyroscoplo pltohlng moments, olovntor up 33°, ballast at nose and tail Thus far in the computations, only one ballast putations already described. This was for the case condition…
NASA Technical Reports Server (NTRS)
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