If the buffer airfoil has an excessively coarse point spacing, additional points can be added with the CADD command. In either of these cases, GSET is skipped. It typically contains coordinates read in from a disk file by LOAD at Top Level, or coordinates generated by EXEC from the MDES menu, depending on what was done last. Sometimes it might be desired to operate directly on the coordinates of an already existing buffer airfoil. The first command typically executed is GSET, which sets the temporary buffer airfoil from the current airfoil. Wind Plot window adjust via cursor and keys INPL Replot buffer airfoil without scaling (in inches) Add points at corners exceeding angle threshold UNIT Normalize buffer airfoil to unit chordĭist Determine distance between 2 cursor pointsĬADD ri. SLOP Toggle modified-contour slope matching flagĬORN Double point with cursor (set sharp corner) CAMB Modify camber shape directly or via loadingīEND Display structural properties of buffer airfoil HIGH rr Move camber and thickness highpoints TFAC rr Scale existing thickness and camber TCPL Toggle thickness and camber plotting GSET Set buffer airfoil <= current airfoilĮXec Set current airfoil <= buffer airfoil
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