Draft: importAirfoilDAT, removed excessive whitespace
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@@ -98,7 +98,7 @@ def open(filename):
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process(doc, filename)
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def insert(filename,docname):
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def insert(filename, docname):
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"""Get an active document and parse.
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If no document exists, it is created.
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@@ -152,18 +152,17 @@ def process(doc, filename):
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afile = pythonopen(filename, 'r')
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# read the airfoil name which is always at the first line
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airfoilname = afile.readline().strip()
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coords = []
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upside = True
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last_x = None
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# Collect the data for the upper and the lower side separately if possible
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for lin in afile:
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curdat = regex.match(lin)
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if curdat is not None:
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x = float(curdat.group("xval"))
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y = float(curdat.group("yval"))
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@@ -173,27 +172,24 @@ def process(doc, filename):
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# End of if curdat != None
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# End of for lin in file
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afile.close()
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if len(coords) < 3:
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print('Did not find enough coordinates\n')
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return
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return
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# sometimes coords are divided in upper an lower side
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# so that x-coordinate begin new from leading or trailing edge
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# check for start coordinates in the middle of list
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if coords[0:-1].count(coords[0]) > 1:
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flippoint = coords.index(coords[0],1)
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flippoint = coords.index(coords[0], 1)
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upper = coords[0:flippoint]
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lower = coords[flippoint+1:]
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lower.reverse()
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for i in lower:
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upper.append(i)
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upper.append(i)
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coords = upper
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# do we use the parametric Draft Wire?
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if useDraftWire:
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obj = makeWire(coords, True)
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@@ -207,22 +203,22 @@ def process(doc, filename):
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if first_v == None:
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first_v = v
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# End of if first_v == None
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# Line between v and last_v if they're not equal
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if (last_v is not None) and (last_v != v):
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lines.append(Part.makeLine(last_v, v))
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lines.append(Part.makeLine(last_v, v))
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# End of if (last_v != None) and (last_v != v)
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# The new last_v
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last_v = v
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last_v = v
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# End of for v in upper
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# close the wire if needed
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if last_v != first_v:
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lines.append(Part.makeLine(last_v, first_v))
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# End of if last_v != first_v
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wire = Part.Wire(lines)
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face = Part.Face(wire)
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obj = FreeCAD.ActiveDocument.addObject('Part::Feature',airfoilname)
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face = Part.Face(wire)
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obj = FreeCAD.ActiveDocument.addObject('Part::Feature',airfoilname)
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obj.Shape = face
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doc.recompute()
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