Wing profile for an axial flow compressor comprises an inner arc surface and an arc crest for distributing a flow speed having an ultrasonic maximum value within a specified region on a chord from the leading edge

摘要

Wing profile comprises an inner arc surface and an arc crest for distributing a flow speed having an ultrasonic maximum value within a region up to 6 % on a chord from the leading edge. Preferred Features: The ultrasound region in the distribution of the flow speed on the chord of the arc crest is delimited within the region of up to 15 % on the chord of the leading edge.