![]() This report is the user's guide to operation of COMOC for the aerodynamics sequence.Ĭomputer programs for calculating two-dimensional potential flow through deflected nozzlesĬomputer programs to calculate the incompressible potential flow, corrected for compressibility, in two-dimensional nozzles at arbitrary operating conditions are presented. By sequencing through these options, it is possible to computationally construct a weak-interaction model of the aerodynamic flowfield. These include the potential flow option, the boundary layer option, and the parabolic Navier-Stokes option. The sequence is constituted of three specific flowfield options in COMOC for two dimensional flows. The two dimensional aerodynamics sequence was established for solution of the potential and/or viscous and turbulent flowfields associated with subsonic flight of elementary two dimensional isolated airfoils. The COMOC finite element fluid mechanics computer program system is applicable to diverse problem classes. COMOC 2: Two-dimensional aerodynamics sequence, computer program user's guide
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