Overview of requested data to be reported: Case 1 (HL-CRM): Note: the semispan HL-CRM is defined in the +Y plane; all CP/CF cuts and velocity lines assume this alignment Forces & moment - CL, CD, and CM as a function of grid size for case 1a (or as a function of adaption for case 1b) for alpha=8 and 16 - CL, CD, and CM on medium grid for case 1c (or on adapted grid for case 1d) for alpha=8 and 16 - PURPOSE: learn trends with grid refinement and compare full gap results with partial seal results Cp & Cf data - Cp and optional Cf on 8 spanwise cuts on the wing - includes multiple grids for cases 1a and 1b - There are no experimental data yet, but these spanwise cuts are estimated locations for when the model is built (the final model will likely have the rows defined when in stowed positions, but here we are asking for y=constant cuts over all elements in their DEPLOYED positions, for simplicity, since the actual locations are not known yet) - PURPOSE: compare solutions between participants, also learn trends with grid refinement (cases 1a and 1b) Iterative histories - Forces, moment, and optional residuals as a function of iteration - PURPOSE: establish how well converged solutions are Velocity profiles - velocity along 6 lines over the wing - PURPOSE: learn trends with grid refinement, especially regarding resolution of the wakes from upstream elements and learn differences between full gap and partial seal flap configs Case 2 (JSM): Note: the semispan JSM is defined in the -Y plane; all CP/CF cuts and velocity lines assume this alignment Forces & Moment - CL, CD, and CM for 6 alphas, both with and without nacelle/pylon - PURPOSE: compare lift, drag, and moment curves with experiment (w and w/o nacelle/pylon) Cp & Cf data - Cp and optional Cf on 7 spanwise cuts on the wing and one on the fuselage - PURPOSE: compare Cp solutions with experiment (w and w/o nacelle/pylon) Iterative histories - Forces, moment, and optional residuals as a function of iteration - PURPOSE: establish how well converged solutions are Velocity profiles - velocity along 2 lines over the wing - PURPOSE: compare profiles between participants Case 3 (2D Verification Study): Grid Convergence info - CL, CD, CDp, CDv, and min U velocities at 2 x/c stations as a function of grid size - PURPOSE: learn trends with grid refinement, compare with others using the same turbulence model Velocity and turbulent shear stress profiles - extracted along 7 x/c stations in the wake - PURPOSE: compare with experiment & other CFD results Cp data - Cp vs. x/c on the airfoil - PURPOSE: compare with other CFD results Iterative histories - Forces and optional residuals as a function of iteration - PURPOSE: establish how well converged solutions are