THE EXPERIMENTS WERE CONDUCTED IN SEVERAL WIND TUNNELS WITH FREESTREAM MACH NUMBERS RANGING FROM 2 TO 6 AND UNIT REYNOLDS NUMBERS OF (10 TO 60) BY 1,000,000/M. IN THIS RANGE OF FLOW PARAMETERS, A QUALITATIVE CORRELATION WAS OBSERVED IN THE CHANGES IN TRANSITION REYNOLDS NUMBER AND PRESSURE PULSATIONS WITH INCREASING UNIT REYNOLDS NUMBER. A CORRELATION PARAMETER ACCOUNTING FOR THE INTENSITY AND SCALE OF DISTURBANCES IS PROPOSED FOR GENERALIZING AVAILABLE EXPERIMENTAL DATA. IT IS SHOWN THAT THE EFFECT OF THE UNIT REYNOLDS NUMBER IS EQUIVALENT TO THE COMBINED INFLUENCE OF ACOUSTIC DISTURBANCES AND OF THE LEADING-EDGE BLUNTNESS OF THE MODEL ON TRANSITION.