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advanced transport configuration agreement with experiment angle of attack boundary conditions boundary-layer code chord line chordwise pressure distributions computed continuity equation converging an interacted coordinate system cove region pressure decambering described in reference developed displacement body displacement surface experimental data external streamline fine-grid iterations FULL WAKE MODEL full-potential equation integral boundary-layer method integral equations integral method integral parameters interaction procedure inviscid calculation inviscid flow laminar Langley Research Center lift coefficient lift distribution lift reduction lower surface cove Mach number midspan momentum equations Navier-Stokes equations ORIGINAL WAKE MODEL potential jump required to converge Reynolds number shock spanwise derivatives streamwise direction streamwise shape factor strong interaction supercritical supercritical airfoil Supercritical wings surface cove region surface normal test case configuration three-dimensional boundary-layer three-dimensional integral boundary-layer three-dimensional wing tion trailing edge trailing-edge angle transonic turbulent two-dimensional strip upper surface viscous correction viscous effects wake curvature effects wake displacement wing surface wing-body configurations