Flight tests for the determination of static longitudinal stability (1930)
NASA Technical Reports Server (NTRS) · leaf 13
.positions 0, Airplane minus additional rv-12 4 weights. 1, Airplane with sliding weight; front and tank H empty. ,7- 0 .. n Wing chord Airplane with sliding weight rear and tank empty 3, ! " " n front. » " f,,!! front full . 4- l' If ti it *» " rear ii Fig.4 CP. positions (scale 1:30) Sliding… … -6° -4° -2° 0° 2° 4° ' 6° 8° 10° Fig.6 Calibration curve of elevator setting'recorder,
NASA Technical Reports Server (NTRS)
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