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Macro ImportAirfoil

{{Macro |Name=ImportAirfoil |Description=Macro for Airfoil coordinates import. |Author=Miloš Petrašinović |Download=[https://wiki.freecadweb.org/File:ImportAirfoil.svg ToolBar Icon] |Date=2022-01-08 |Version=1.0.0 |FCVersion=0.18.4 and above |SeeAlso=[https://github.com/VAZMFB/FreeCAD-ImportAirfoil Github repository] }}

Description

Macro for Airfoil coordinates import. It is possible, using simple dialog, to scale the airfoil, rotate, translate in the plane, translate along the span, select the plane and the main axis, as well as turn the geometry into a sketch. It is possible to import coordinates saved in the most commonly used formats.

Usage

Run the macro program and follow the instructions.

Script

ToolBar Icon

ImportAirfoil.FCMacro

{{MacroCode|code=

Airfoil import macro

After selecting the file with the coordinates of the airfoil

data processing and modeling of the airfoil are performed.

It is possible, using simple dialog, to scale the airfoil, rotate,

translate in the plane, translate along the span, select the plane and

the main axis, as well as turn the geometry into a sketch. It is possible

to import coordinates saved in the most commonly used formats.

Airfoil import is based on:

Author: Milos D. Petrasinovic mpetrasinovic@mas.bg.ac.rs

Structural Analysis of Flying Vehicles

Faculty of Mechanical Engineering, University of Belgrade

Department of Aerospace Engineering, Flying structures

Belgrade, 2022

--------------------

Copyright (C) 2022 Milos Petrasinovic info@vazmfb.com

This program is free software: you can redistribute it and/or modify

it under the terms of the GNU Lesser General Public License as

published by the Free Software Foundation, either version 3 of the

License, or (at your option) any later version.

This program is distributed in the hope that it will be useful,

but WITHOUT ANY WARRANTY; without even the implied warranty of

MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the

GNU Lesser General Public License for more details.

You should have received a copy of the GNU Lesser General Public License

along with this program. If not, see https://www.gnu.org/licenses/.

--------------------

Based on:

Airfoil Import and Scale 2.1.2

(c) quick61

--------------------

Name = 'ImportAirfoil' Comment = 'Airfoil import macro' Author = 'Milos Petrasinovic mpetrasinovic@mas.bg.ac.rs' Version = '1.0.0' Date = '2022-01-06' License = 'GPL-3.0-or-later' Web = 'https://github.com/VAZMFB/FreeCAD-ImportAirfoil' Wiki = 'https://wiki.freecadweb.org/Macro_ImportAirfoil' Icon = 'ImportAirfoil.svg' Help = 'Run the macro program and follow the instructions!' Status = 'stable' Requires = 'Freecad >= 0.19' Communication = 'https://github.com/VAZMFB/FreeCAD-ImportAirfoil/issues/' Files = 'ImportAirfoil.svg'

import FreeCAD as App from PySide import QtCore, QtGui from PySide.QtGui import QFileDialog, QLineEdit, QRadioButton, QMessageBox import Draft, importAirfoilDAT import numpy as np import subprocess import sys import os import re

global filename global nameFile

msgBox = QtGui.QMessageBox() msgBox.setWindowTitle("ImportAirfoil") msgBox.setText("In the next window, select the file with the coordinates of the airfoil.") msgBox.exec_()

try: filename, filefilter = QtGui.QFileDialog.getOpenFileName(QtGui.qApp.activeWindow(), 'Select the file with the coordinates:', '.dat;.txt;.af') except Exception: param = FreeCAD.ParamGet("User parameter:BaseApp/Preferences/Macro") path = param.GetString("MacroPath", "") + "/" filename, filefilter = QFileDialog.getOpenFileName(None, "Select the file with the coordinates:", path, ".dat;.txt;.af")

nameFile = filename.split("/")[-1][:-4]

class DrawAP(): def init(self): self.dialog = None self.lt = 0 self.alpha = 0 self.h0 = 0 self.plane = None self.mirror = None self.dh = 0 self.dv = 0 self.db = 0 self.sketch = None

    # Dialog window
    self.dialog = QtGui.QDialog()
    self.dialog.resize(350, 100)
    self.dialog.setWindowTitle("ImportAirfoil")
    la = QtGui.QVBoxLayout(self.dialog)
    tx = QtGui.QLabel("Length of airfoil chord [mm]:")
    la.addWidget(tx)
    self.lt = QtGui.QLineEdit("1000")
    la.addWidget(self.lt)
    tx = QtGui.QLabel("The angle of rotation [deg]:")
    la.addWidget(tx)
    self.alpha = QtGui.QLineEdit("0")
    la.addWidget(self.alpha)
    tx = QtGui.QLabel("The relative position of the axis of rotation [% of chord]:")
    la.addWidget(tx)
    self.h0 = QtGui.QLineEdit("25")
    la.addWidget(self.h0)
    tx = QtGui.QLabel("Plane selection [XY = 1, YZ = 2, ZX = 3]:")
    la.addWidget(tx)
    self.plane = QtGui.QLineEdit("1")
    la.addWidget(self.plane)
    tx = QtGui.QLabel("Vertical mirroring [NO = 0, YES = 1]:")
    la.addWidget(tx)
    self.mirror = QtGui.QLineEdit("0")
    la.addWidget(self.mirror)
    tx = QtGui.QLabel("Change axis [NO = 0, YES = 1]:")
    la.addWidget(tx)
    self.flip = QtGui.QLineEdit("0")
    la.addWidget(self.flip)
    tx = QtGui.QLabel("Translation along the horizontal axis [mm]:")
    la.addWidget(tx)
    self.dh = QtGui.QLineEdit("0")
    la.addWidget(self.dh)
    tx = QtGui.QLabel("Translation along the vertical axis [mm]:")
    la.addWidget(tx)
    self.dv = QtGui.QLineEdit("0")
    la.addWidget(self.dv)
    tx = QtGui.QLabel("Translation along the span [mm]:")
    la.addWidget(tx)
    self.db = QtGui.QLineEdit("0")
    la.addWidget(self.db)
    tx = QtGui.QLabel("Create a Sketch [NO = 0, YES = 1]:")
    la.addWidget(tx)
    self.sketch = QtGui.QLineEdit("0")
    la.addWidget(self.sketch)

    # Add OK / Cancel buttons
    okBox = QtGui.QDialogButtonBox(self.dialog)
    okBox.setOrientation(QtCore.Qt.Horizontal)
    okBox.setStandardButtons(QtGui.QDialogButtonBox.Cancel|QtGui.QDialogButtonBox.Ok)
    la.addWidget(okBox)
    QtCore.QObject.connect(okBox, QtCore.SIGNAL("accepted()"), self.proceed)
    QtCore.QObject.connect(okBox, QtCore.SIGNAL("rejected()"), self.close)
    QtCore.QMetaObject.connectSlotsByName(self.dialog)
    self.dialog.show()
    self.dialog.exec_()

def proceed(self):
    global filename
    global nameFile
    try:
        lt = float(self.lt.text())
        alpha = float(self.alpha.text())
        h0 = float(self.h0.text())
        plane = float(self.plane.text())
        mirror = float(self.mirror.text())
        flip = float(self.flip.text())
        dh = float(self.dh.text())
        dv = float(self.dv.text())
        db = float(self.db.text())
        sketch = float(self.sketch.text())
        af = importAirfoil(str(filename))
        
        # Open trailing edge
        af[1][0] += 0.000001;
        points = []
        for i in range(len(af[0])):
            point = App.Vector(af[0][i], af[1][i], 0)
            points.append(point)
        
        Line1 = Draft.makeLine(points[0], points[-1])
        Line1.Label = nameFile + "_(TEdge)"
        BSpline1 = Draft.makeBSpline(points, closed=False)
        BSpline1.Label = nameFile + "_(BSpline)"

        # Group elements
        Group1 = App.activeDocument().addObject('App::DocumentObjectGroup', 'Group')
        Group1.Label = nameFile + "_(Group)"
        Group1.addObject(Line1)
        Group1.addObject(BSpline1)

        App.activeDocument().recompute()

        # Scale airfoil
        if App.Version()[1] < "19":
            Draft.scale([Line1, BSpline1], App.Vector(lt, lt, lt), center=App.Vector(0.0, 0.0, 0.0), copy=False, legacy=True)
        else:
            Draft.scale([Line1, BSpline1], App.Vector(lt, lt, lt), center=App.Vector(0.0, 0.0, 0.0), copy=False)

        # Rotate airfoil
        Draft.rotate([Line1, BSpline1], -alpha, center=App.Vector(lt*h0/100, 0, 0), axis=App.Vector(0, 0, 1), copy=False)
        
        # Mirror
        if mirror == 1:
            Draft.rotate([Line1, BSpline1], 180, center=App.Vector(0, 0, 0), axis=App.Vector(0, 1, 0), copy=False)

        # Move airfoil in plane
        Draft.move([Line1, BSpline1], App.Vector(dh, dv, 0.0), copy=False)
            
        # Change axis
        Draft.rotate([Line1, BSpline1], -90, center=App.Vector(0, 0, 0), axis=App.Vector(0, 0, 1), copy=False)
        
        # Change plane
        if plane == 2: # YZ
            Draft.rotate([Line1, BSpline1], 90, center=App.Vector(0, 0, 0), axis=App.Vector(0, 0, 1), copy=False)
            Draft.rotate([Line1, BSpline1], 90, center=App.Vector(0, 0, 0), axis=App.Vector(0, 1, 0), copy=False)
        elif plane == 3: # ZX
            Draft.rotate([Line1, BSpline1], 90, center=App.Vector(0, 0, 0), axis=App.Vector(1, 0, 0), copy=False)
            Draft.rotate([Line1, BSpline1], -90, center=App.Vector(0, 0, 0), axis=App.Vector(0, 1, 0), copy=False)

        # Make sketch
        if sketch == 1:
            App.activeDocument().recompute()
            Sketch1 = Draft.makeSketch([Line1, BSpline1], autoconstraints=True)
            Sketch1.Label = nameFile + "_(Sketch)"

        # Move airfoil
        if plane == 2: # YZ
            Draft.move([Line1, BSpline1], App.Vector(db, 0, 0), copy=False)
            if sketch == 1:
                Draft.move(Sketch1, App.Vector(0, 0, db), copy=False)
        elif plane == 3: # ZX
            Draft.move([Line1, BSpline1], App.Vector(0, db, 0), copy=False)
            if sketch == 1:
                Draft.move(Sketch1, App.Vector(0, 0, db), copy=False)
        else:
            Draft.move([Line1, BSpline1], App.Vector(0, 0, db), copy=False)
            if sketch == 1:
                Draft.move(Sketch1, App.Vector(0, 0, db), copy=False)
                
    except Exception as e:
          exc_type, exc_obj, exc_tb = sys.exc_info()
          App.Console.PrintError("Error = "+str(e)+"\n")
          App.Console.PrintError("    Error line number = "+str(exc_tb.tb_lineno)+"\n")
          msgBox = QtGui.QMessageBox()
          msgBox.setWindowTitle("Error")
          msgBox.setText("An error occurred, see Report window for more information!")
          msgBox.setWindowModality(QtCore.Qt.NonModal)
          msgBox.show()

    App.activeDocument().recompute()
    Gui.SendMsgToActiveView("ViewFit")
    self.close() # close the window
    
def close(self):
    self.dialog.hide() # close the window

def scanf(l): # scanf('%f %f', l) found = re.compile('([-+]?(?:\d+(?:\.\d*)?|\.\d+)(?:[eE][-+]?\d+)?)\s+([-+]?(?:\d+(?:\.\d*)?|\.\d+)(?:[eE][-+]?\d+)?)').search(l) casts = [float, float] if found: groups = found.groups() return tuple([castsi for i in range(len(groups))])

def importAirfoil(file): af = []; if(os.path.isfile(file)): with open(file) as f: ls = [line.strip() for line in f]

    x = []
    y = []
    h = 1
    for l in ls:
        if l:
            data = scanf(l);
            if(h and data and len(data) == 2 and data[0] > -0.1
                    and data[0] < 1.1 and data[1] > -1.1 
                    and data[1] < 1.1):
                # First coordinate if there is both x and y data
                # Range for x is [-0.1, 1.1] and for y is [-1.1, 1.1]
                h = 0;
                x.append(data[0])
                y.append(data[1])
            elif(not h and data and len(data) == 2):
                x.append(data[0])
                y.append(data[1])
    
    if(len(x) > 0):
        if(any(xi >= 1.1 for xi in x)):
            # Koordinate su verovatno pomnozene sa 100
            x = np.divide(x, 100)
            y = np.divide(y, 100)
                  
    d = np.diff(x)
    if(sum([di < 0 for di in d]) == 1):
        # Lednicer format
        i = np.where(d < 0)[0][0]
        x = [*np.flip(x[:i+1]).tolist(), *x[i+1:]]
        y = [*np.flip(y[:i+1]).tolist(), *y[i+1:]]

    af = np.array([x[1:-1], y[1:-1]])
    _, idx = np.unique(af, axis=1, return_index=True)
    af = [[x[0], *af[0][np.sort(idx)].tolist(), x[-1]],
        [y[0], *af[1][np.sort(idx)].tolist(), y[-1]]]
return af

if os.path.isfile(filename): DrawAP() else: msgBox = QtGui.QMessageBox() msgBox.setWindowTitle("Error") msgBox.setText("No valid file with coordinates!") msgBox.setWindowModality(QtCore.Qt.NonModal) msgBox.show() }}

Links

The forum discussion New Macro: ImportAirfoil


documentation index > Macro ImportAirfoil