Angles of Attack and Air Speeds During Maneuvers (1921)
NASA Technical Reports Server (NTRS) · leaf 10
38 per cent larger than the mean loading. The load factor given by the curve is 1.25, which is somewhat smaller than the load factor found with an accelerometer in similar spins. It is probable that the principal cause of the discrepancies lies in the fact that the ailerons are not centered, and… … +/6 +20 +22 -32-20 -/6 -t'2 -6 -4 O +4 +8 +/2 D/stonce from P/one of Symmetry /n Feet. Fig, 7. uniformly It will be noted in figure 7 that the resultant speed does not by any means vary along the wing, but falls off to a minimum just beyond the inner strut on the inner wing and then increases again…
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