コード例 #1
0
ファイル: profile_2d.py プロジェクト: luzpaz/OpenGlider
 def numpoints(self, numpoints):
     self.x_values = Distribution.from_cos_distribution(numpoints)
コード例 #2
0
ファイル: glider.py プロジェクト: luzpaz/OpenGlider
    def get_glider_3d(self, glider=None, num=50, num_profile=None):
        """returns a new glider from parametric values"""
        glider = glider or Glider()
        ribs = []

        self.rescale_curves()

        x_values = self.shape.rib_x_values
        shape_ribs = self.shape.ribs

        profile_merge_curve = self.profile_merge_curve.interpolation(num=num)
        ballooning_merge_curve = self.ballooning_merge_curve.interpolation(
            num=num)
        aoa_int = self.aoa.interpolation(num=num)
        zrot_int = self.zrot.interpolation(num=num)

        arc_pos = list(self.arc.get_arc_positions(x_values))
        rib_angles = self.arc.get_rib_angles(x_values)

        if self.num_profile is not None:
            num_profile = self.num_profile

        if num_profile is not None:
            profile_x_values = Distribution.from_cos_distribution(num_profile)
        else:
            profile_x_values = self.profiles[0].x_values

        rib_holes = self.elements.get("holes", [])
        rigids = self.elements.get("rigidfoils", [])

        cell_centers = [(p1 + p2) / 2
                        for p1, p2 in zip(x_values[:-1], x_values[1:])]
        offset_x = shape_ribs[0][0][1]
        for rib_no, pos in enumerate(x_values):
            front, back = shape_ribs[rib_no]
            arc = arc_pos[rib_no]
            startpoint = np.array([-front[1] + offset_x, arc[0], arc[1]])

            chord = abs(front[1] - back[1])
            factor = profile_merge_curve(abs(pos))
            profile = self.get_merge_profile(factor)
            profile.name = "Profile{}".format(rib_no)
            profile.x_values = profile_x_values

            this_rib_holes = [
                RibHole(ribhole["pos"], ribhole["size"])
                for ribhole in rib_holes if rib_no in ribhole["ribs"]
            ]
            this_rigid_foils = [
                RigidFoil(rigid["start"], rigid["end"], rigid["distance"])
                for rigid in rigids if rib_no in rigid["ribs"]
            ]

            ribs.append(
                Rib(profile_2d=profile,
                    startpoint=startpoint,
                    chord=chord,
                    arcang=rib_angles[rib_no],
                    glide=self.glide,
                    aoa_absolute=aoa_int(pos),
                    zrot=zrot_int(pos),
                    holes=this_rib_holes,
                    rigidfoils=this_rigid_foils,
                    name="rib{}".format(rib_no)))
            ribs[-1].aoa_relative = aoa_int(pos)

        if self.shape.has_center_cell:
            new_rib = ribs[0].copy()
            new_rib.name = "rib0"
            new_rib.mirror()
            new_rib.mirrored_rib = ribs[0]
            ribs.insert(0, new_rib)
            cell_centers.insert(0, 0.)

        glider.cells = []
        for cell_no, (rib1, rib2) in enumerate(zip(ribs[:-1], ribs[1:])):
            ballooning_factor = ballooning_merge_curve(cell_centers[cell_no])
            ballooning = self.merge_ballooning(ballooning_factor)
            cell = Cell(rib1, rib2, ballooning, name="c{}".format(cell_no + 1))

            glider.cells.append(cell)

        glider.close_rib()

        # CELL-ELEMENTS
        self.get_panels(glider)
        self.apply_diagonals(glider)

        for minirib in self.elements.get("miniribs", []):
            data = minirib.copy()
            cells = data.pop("cells")
            for cell_no in cells:
                glider.cells[cell_no].miniribs.append(MiniRib(**data))

        # RIB-ELEMENTS
        #self.apply_holes(glider)

        glider.rename_parts()

        glider.lineset = self.lineset.return_lineset(glider, self.v_inf)
        glider.lineset.glider = glider
        glider.lineset.calculate_sag = False
        for _ in range(3):
            glider.lineset.recalc()
        glider.lineset.calculate_sag = True
        glider.lineset.recalc()

        return glider