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Timing Data for Scalar and Vector Versions of the Propfan Euler Code
A The Files Used for Data Transfer Among Various Segments of the Program
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1-80 Header card AIAA airfoil Boeing Commercial Airplane boundary condition boundary layer chord coarsest mesh common boundary computational domain configuration Control Data Corporation counter CYBER Displacement Thickness downstream Euler Equations exhaust flow exhaust plume field is left Flow Grid flowfield flux fuselage geometry grid cells grid embedding grid generation program grid planes inboard input cards input file inviscid JOB CONTROL DECK leading edge lower section curve Mach number method nacelle is present nacelle surface Name Description nondimensionalized nonzero number of cells Number of grid Number of points Parameter specifying physical plane plane of interest plane that user PRGRD11 program will default Propeller Disk Propfan PRPOST pusher pusher configuration Recommended value region SAMANT simulated specifying the presence step 1a TAPE2 TAPE4 tractor tractor configuration Transonic Turboprop upper section curve user wishes vector velocity volume grid wing section wing surface grid Wing-Mounted wishes to extract y/c coordinate YSYM