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AEDC 16T aerodynamic airfoil angle of attack chord chordwise location COMPOSITE CORRELATION correlated separation development correlation curves correlation parameter CPTE CPTEO and B1/2 data to flight defined development of trailing-edge effective angle extrapolation procedure F-8 SCW Figure 48 FINAL CORRELATION flight data flight Reynolds number FLIGHT RN flight test high Reynolds number high speed transport INITIAL CORRELATION J. F. Cahill Lockheed-Georgia Company low Reynolds number NASA number and angle parameter B1/2 parameter P15 peak negative pressure Pearcey planform PLATEAU PRESSURE plotted PML FIGURE pressure distribution data RAE Model 864 Reynolds number changes scale effect curves semispan model separation criteria shock pressure rise shown in Figure single curve supercritical wings swept wing terminal shock trailing edge separation trailing-edge pressure coefficient trailing-edge pressure recovery trailing-edge separation transonic tunnel and flight value of CPSH values of B1/2 variation of trailing-edge vortex wind tunnel data WT WT WT XCSH