Abstract
Proposed is a method of zero load approximation on scale 6KETB in wind tunnel ТАД-2 of Kyiv International University of Civil Aviation which guarantees the increase of operation efficiency of the airdynamic experiment and reduction of experiment time by 30-50 %. Considered is the load hysteresis due to angle change of placing the object of investigation. It is proved that its influence on the measurement error can be neglected
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