Correlation of Turbofan Engine Thrust Performance with Comnound Nozzle Flow Theorv

from a very short data sample, the average value should be computed, giving /**. Then the standard deviation flow conditions from the following relations: subcritical: Kmax = 30* + ju^; critical: Kmax = 3.50-fc + /zfc; supercritical: Krnax = 5.5(7* + /A*; where K represents this distortion parameter.