Correlation of data related to shock-induced trailing-edge separation and extrapolation to flight Reynolds numberNational Aeronautics and Space Administration, Scientific and Technical Information Branch, 1979 - Aerodynamic load - 79 pages |
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1.0 X/C FIGURE AEDC 16T aerodynamic airfoil angle of attack B1/2 FIGURE boundary layer chord chordwise location COMPOSITE CORRELATION correlated separation development correlation curves correlation parameter CPTE CPTE CPTE-CPTEO CPTEO and B1/2 data to flight defined development of trailing-edge effective angle ERDOS extrapolation procedure F-8 SCW Figure 46 FINAL CORRELATION flight data flight Reynolds number high Reynolds number high speed transport INITIAL CORRELATION J. F. Cahill leading edge Lockheed-Georgia Company low Reynolds number NASA parameter B1/2 parameter P15 plotted pressure distribution data RAE MODEL 864 Reynolds number changes RMAC semispan model shock location shock pressure rise shown in Figure single curve SOURCE RN-106 SYM supercritical wings swept wing terminal shock trailing edge separation trailing-edge pressure coefficient trailing-edge pressure recovery trailing-edge separation transonic tunnel and flight TYPICAL PRESSURE DISTRIBUTIONS value of CPSH values of B1/2 variation of trailing-edge vortex wind tunnel data Ср