iT.A.CA, Technical Memorand-um 110.684 Figs.3,4 2 0 10 20 30 Seconds Pig. 3 The saiae coefficient (x as in Pigore 2, "but here plotted against time, in the case of a maneuver at constant lift (curve 2 of fig.2). … 1 2 3 4 5 Pig.4 Propeller thrust plotted against speed range. The ahscissa represents the speed range, i.e. the ratio of the maximum speed to the landing speed. It is expressed by the formulav^G^m/c^ - which C^M represents the majcimum value of Og.
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