コード例 #1
0
 def test_random_allowables(self):
     rc = 0.15
     num = 4
     bearing = [0, 0]
     bypass = [1000., 0., 0.]
     analysis = MaxStrain(QUASI,
                          QUASI_THICK,
                          DIAMETER,
                          et={0: QUASI_UNT},
                          ec={90: QUASI_UNC})
     margins = analysis.analyze(bearing, bypass, rc=rc, num=num)
     strains = analysis.strains(bearing, bypass, rc=rc, num=num)
     compare_margins = np.empty((num, 4))
     with np.errstate(divide='ignore'):
         # axial strains
         x_strains = strains[:, 0]
         compare_margins[:, 0] = np.select(
             [x_strains > 0, x_strains < 0],
             [QUASI_UNT / x_strains - 1, -np.inf / x_strains - 1])
         # shear strains
         xy_strains = np.abs(strains[:, 2])
         compare_margins[:, 1] = np.inf / xy_strains - 1
         rotated_strains = rotate_strains(strains, angle=np.deg2rad(90))
         # axial strains
         x_strains = rotated_strains[:, 0]
         compare_margins[:, 2] = np.select(
             [x_strains > 0, x_strains < 0],
             [np.inf / x_strains - 1, -abs(QUASI_UNC) / x_strains - 1])
         # shear strains
         xy_strains = np.abs(rotated_strains[:, 2])
         compare_margins[:, 3] = np.inf / xy_strains - 1
     assert_array_almost_equal(margins, compare_margins)
コード例 #2
0
 def setUp(self):
     self.analysis = MaxStrain(
         QUASI,
         QUASI_THICK,
         DIAMETER,
         et0=QUASI_UNT,
         et90=QUASI_UNT,
         et45=QUASI_UNT,
         etn45=QUASI_UNT,
         ec0=QUASI_UNC,
         ec90=QUASI_UNC,
         ec45=QUASI_UNC,
         ecn45=QUASI_UNC,
         es0=QUASI_SBS,
         es90=QUASI_SBS,
         es45=QUASI_SBS,
         esn45=QUASI_SBS,
     )
コード例 #3
0
 def setUp(self):
     self.analysis = MaxStrain(
         QUASI,
         QUASI_THICK,
         DIAMETER,
         et={
             0: QUASI_UNT,
             90: QUASI_UNT,
             45: QUASI_UNT,
             -45: QUASI_UNT
         },
         ec={
             0: QUASI_UNC,
             90: QUASI_UNC,
             45: QUASI_UNC,
             -45: QUASI_UNC
         },
         es={
             0: SHEAR_STRN,
             90: SHEAR_STRN,
             45: SHEAR_STRN,
             -45: SHEAR_STRN
         },
     )
コード例 #4
0
 def test_equalize_dicts(self):
     analysis = MaxStrain(
         QUASI,
         QUASI_THICK,
         DIAMETER,
         et={
             0: QUASI_UNT,
             30: QUASI_UNT
         },
         ec={
             90: QUASI_UNC,
             60: QUASI_UNC
         },
         es={45: SHEAR_STRN},
     )
     self.assertTrue(
         analysis.et.keys() == analysis.ec.keys() == analysis.es.keys())
     self.assertAlmostEquals(analysis.et[0], QUASI_UNT)
     self.assertAlmostEquals(analysis.et[30], QUASI_UNT)
     self.assertAlmostEquals(analysis.ec[90], QUASI_UNC)
     self.assertAlmostEquals(analysis.ec[60], QUASI_UNC)
     self.assertAlmostEquals(analysis.es[45], SHEAR_STRN)
     self.assertEqual(analysis.et[90], np.inf)
コード例 #5
0
class TestMaxStrainQuasi(unittest.TestCase):
    def setUp(self):
        self.analysis = MaxStrain(
            QUASI,
            QUASI_THICK,
            DIAMETER,
            et0=QUASI_UNT,
            et90=QUASI_UNT,
            et45=QUASI_UNT,
            etn45=QUASI_UNT,
            ec0=QUASI_UNC,
            ec90=QUASI_UNC,
            ec45=QUASI_UNC,
            ecn45=QUASI_UNC,
            es0=QUASI_SBS,
            es90=QUASI_SBS,
            es45=QUASI_SBS,
            esn45=QUASI_SBS,
        )

    def test_xy_points(self):
        rc = 0.
        num = 4
        x, y = self.analysis.xy_points(rc=rc, num=num)
        radius = DIAMETER / 2
        self.assertAlmostEqual(x[0], radius)
        self.assertAlmostEqual(x[1], 0.)
        self.assertAlmostEqual(x[2], -radius)
        self.assertAlmostEqual(x[3], 0.)
        self.assertAlmostEqual(y[0], 0.)
        self.assertAlmostEqual(y[1], radius)
        self.assertAlmostEqual(y[2], 0.)
        self.assertAlmostEqual(y[3], -radius)

    def test_strain_rotation(self):
        bearing = [0, 0]
        bypass = [100, 0, 0]
        angles = [np.deg2rad(45.), np.deg2rad(-45.)]
        for angle in angles:
            rotated_stresses = rotate_plane_stress(self.analysis.stresses(
                bearing, bypass),
                                                   angle=angle)
            assert_array_almost_equal(
                (self.analysis.a_inv
                 @ (rotated_stresses * self.analysis.t).T).T,
                self.analysis._rotate_strains(self.analysis.strains(
                    bearing, bypass),
                                              angle=angle),
            )

    def test_0_bearing_0_angle(self):
        bearing = [0, 0]
        p, theta = self.analysis.bearing_angle(bearing)
        self.assertAlmostEqual(p, 0.)
        self.assertAlmostEqual(np.rad2deg(theta), 0.)

    def test_bearing_0_angle(self):
        bearing = [100, 0]
        p, theta = self.analysis.bearing_angle(bearing)
        self.assertAlmostEqual(p, 100.)
        self.assertAlmostEqual(np.rad2deg(theta), 0.)

    def test_bearing_90_angle(self):
        bearing = [0, 100]
        p, theta = self.analysis.bearing_angle(bearing)
        self.assertAlmostEqual(p, 100.)
        self.assertAlmostEqual(np.rad2deg(theta), 90.)

    def test_bearing_180_angle(self):
        bearing = [-100, 0]
        p, theta = self.analysis.bearing_angle(bearing)
        self.assertAlmostEqual(p, 100.)
        self.assertAlmostEqual(np.rad2deg(theta), 180.)

    def test_bearing_n90_angle(self):
        bearing = [0, -100]
        p, theta = self.analysis.bearing_angle(bearing)
        self.assertAlmostEqual(p, 100.)
        self.assertAlmostEqual(np.rad2deg(theta), -90.)

    def test_bearing_45_angle(self):
        bearing = [100, 100]
        p, theta = self.analysis.bearing_angle(bearing)
        self.assertAlmostEqual(p, np.sqrt(np.sum(np.square(bearing))))
        self.assertAlmostEqual(np.rad2deg(theta), 45.)

    def test_width_0_angle(self):
        w = 6 * DIAMETER
        bearing = [100, 0]
        bypass = [0, 0, 0]
        bypass_correction = [100 / (2 * w), 0, 0]
        brg = LoadedHole(bearing[0],
                         DIAMETER,
                         QUASI_THICK,
                         QUASI_INV,
                         theta=0.)
        byp = UnloadedHole(bypass_correction, DIAMETER, QUASI_THICK, QUASI_INV)
        x, y = self.analysis.xy_points(rc=0., num=100)
        byp_stress = byp.stress(x, y)
        brg_stress = brg.stress(x, y)
        total_stress = byp_stress + brg_stress
        analysis_stress = self.analysis.stresses(bearing,
                                                 bypass,
                                                 rc=0.,
                                                 num=100,
                                                 w=w)
        assert_array_almost_equal(total_stress, analysis_stress)

    def test_width_45_angle(self):
        w = 6 * DIAMETER
        bearing = [100, 100]
        bypass = [0, 0, 0]
        p, theta = self.analysis.bearing_angle(bearing)
        bypass_correction = rotate_plane_stress(np.array([p / (2 * w), 0, 0]),
                                                angle=-theta)
        brg = LoadedHole(p, DIAMETER, QUASI_THICK, QUASI_INV, theta=theta)
        byp = UnloadedHole(bypass_correction, DIAMETER, QUASI_THICK, QUASI_INV)
        x, y = self.analysis.xy_points(rc=0., num=100)
        byp_stress = byp.stress(x, y)
        brg_stress = brg.stress(x, y)
        total_stress = byp_stress + brg_stress
        analysis_stress = self.analysis.stresses(bearing,
                                                 bypass,
                                                 rc=0.,
                                                 num=100,
                                                 w=w)
        assert_array_almost_equal(total_stress, analysis_stress)

    def test_max_strain(self):
        rc = 0.15
        num = 4
        bearing = [0, 0]
        bypass = [100., 0., 0.]
        margins = self.analysis.analyze(bearing, bypass, rc=rc, num=num)
        e0, e90, es0 = self.analysis.strains(bearing, bypass, rc=rc,
                                             num=num)[1]
        s0, s90, ss0 = self.analysis.stresses(bearing, bypass, rc=rc,
                                              num=num)[1]
        calc_strains = QUASI_INV @ np.array([s0, s90, ss0]) * QUASI_THICK
        self.assertAlmostEqual(e0, calc_strains[0])
        self.assertAlmostEqual(e90, calc_strains[1])
        self.assertAlmostEqual(es0, calc_strains[2])
        s45, sn45, ss45 = rotate_plane_stress(np.array([s0, s90, ss0]),
                                              angle=np.deg2rad(45.))
        e45, en45, es45 = QUASI_INV @ np.array([s45, sn45, ss45]) * QUASI_THICK
        self.assertAlmostEqual(margins[1, 0], QUASI_UNT / e0 - 1)
        self.assertAlmostEqual(margins[1, 1], -QUASI_UNC / e90 - 1)
        self.assertAlmostEqual(margins[1, 2], QUASI_SBS / abs(es0) - 1)
        self.assertAlmostEqual(margins[1, 3], QUASI_UNT / e45 - 1)
        self.assertAlmostEqual(margins[1, 4], QUASI_UNT / en45 - 1)
        self.assertAlmostEqual(margins[1, 5], QUASI_SBS / abs(es45) - 1)
コード例 #6
0
class TestMaxStrainQuasi(unittest.TestCase):
    def setUp(self):
        self.analysis = MaxStrain(
            QUASI,
            QUASI_THICK,
            DIAMETER,
            et={
                0: QUASI_UNT,
                90: QUASI_UNT,
                45: QUASI_UNT,
                -45: QUASI_UNT
            },
            ec={
                0: QUASI_UNC,
                90: QUASI_UNC,
                45: QUASI_UNC,
                -45: QUASI_UNC
            },
            es={
                0: SHEAR_STRN,
                90: SHEAR_STRN,
                45: SHEAR_STRN,
                -45: SHEAR_STRN
            },
        )

    def test_equalize_dicts(self):
        analysis = MaxStrain(
            QUASI,
            QUASI_THICK,
            DIAMETER,
            et={
                0: QUASI_UNT,
                30: QUASI_UNT
            },
            ec={
                90: QUASI_UNC,
                60: QUASI_UNC
            },
            es={45: SHEAR_STRN},
        )
        self.assertTrue(
            analysis.et.keys() == analysis.ec.keys() == analysis.es.keys())
        self.assertAlmostEquals(analysis.et[0], QUASI_UNT)
        self.assertAlmostEquals(analysis.et[30], QUASI_UNT)
        self.assertAlmostEquals(analysis.ec[90], QUASI_UNC)
        self.assertAlmostEquals(analysis.ec[60], QUASI_UNC)
        self.assertAlmostEquals(analysis.es[45], SHEAR_STRN)
        self.assertEqual(analysis.et[90], np.inf)

    def test_xy_points(self):
        rc = 0.
        num = 4
        x, y = self.analysis.xy_points(rc=rc, num=num)
        radius = DIAMETER / 2
        self.assertAlmostEqual(x[0], radius)
        self.assertAlmostEqual(x[1], 0.)
        self.assertAlmostEqual(x[2], -radius)
        self.assertAlmostEqual(x[3], 0.)
        self.assertAlmostEqual(y[0], 0.)
        self.assertAlmostEqual(y[1], radius)
        self.assertAlmostEqual(y[2], 0.)
        self.assertAlmostEqual(y[3], -radius)

    def test_strain_rotation(self):
        bearing = [0, 0]
        bypass = [100, 0, 0]
        angles = map(np.deg2rad, [0, 45, 90, -45, 60, -60])
        for angle in angles:
            rotated_stresses = rotate_plane_stress(self.analysis.stresses(
                bearing, bypass),
                                                   angle=angle)
            assert_array_almost_equal(
                (self.analysis.a_inv
                 @ (rotated_stresses * self.analysis.t).T).T,
                rotate_strains(self.analysis.strains(bearing, bypass),
                               angle=angle),
            )

    def test_0_bearing_0_angle(self):
        bearing = [0, 0]
        p, theta = self.analysis.bearing_angle(bearing)
        self.assertAlmostEqual(p, 0.)
        self.assertAlmostEqual(np.rad2deg(theta), 0.)

    def test_bearing_0_angle(self):
        bearing = [100, 0]
        p, theta = self.analysis.bearing_angle(bearing)
        self.assertAlmostEqual(p, 100.)
        self.assertAlmostEqual(np.rad2deg(theta), 0.)

    def test_bearing_90_angle(self):
        bearing = [0, 100]
        p, theta = self.analysis.bearing_angle(bearing)
        self.assertAlmostEqual(p, 100.)
        self.assertAlmostEqual(np.rad2deg(theta), 90.)

    def test_bearing_180_angle(self):
        bearing = [-100, 0]
        p, theta = self.analysis.bearing_angle(bearing)
        self.assertAlmostEqual(p, 100.)
        self.assertAlmostEqual(np.rad2deg(theta), 180.)

    def test_bearing_n90_angle(self):
        bearing = [0, -100]
        p, theta = self.analysis.bearing_angle(bearing)
        self.assertAlmostEqual(p, 100.)
        self.assertAlmostEqual(np.rad2deg(theta), -90.)

    def test_bearing_45_angle(self):
        bearing = [100, 100]
        p, theta = self.analysis.bearing_angle(bearing)
        self.assertAlmostEqual(p, np.sqrt(np.sum(np.square(bearing))))
        self.assertAlmostEqual(np.rad2deg(theta), 45.)

    def test_width_0_angle(self):
        w = 6 * DIAMETER
        bearing = [100, 0]
        bypass = [0, 0, 0]
        bypass_correction = [100 / (2 * w), 0, 0]
        brg = LoadedHole(bearing[0],
                         DIAMETER,
                         QUASI_THICK,
                         QUASI_INV,
                         theta=0.)
        byp = UnloadedHole(bypass_correction, DIAMETER, QUASI_THICK, QUASI_INV)
        x, y = self.analysis.xy_points(rc=0., num=100)
        byp_stress = byp.stress(x, y)
        brg_stress = brg.stress(x, y)
        total_stress = byp_stress + brg_stress
        analysis_stress = self.analysis.stresses(bearing,
                                                 bypass,
                                                 rc=0.,
                                                 num=100,
                                                 w=w)
        assert_array_almost_equal(total_stress, analysis_stress)

    def test_width_45_angle(self):
        w = 6 * DIAMETER
        bearing = [100, 100]
        bypass = [0, 0, 0]
        p, theta = self.analysis.bearing_angle(bearing)
        bypass_correction = rotate_plane_stress(np.array([p / (2 * w), 0, 0]),
                                                angle=-theta)
        brg = LoadedHole(p, DIAMETER, QUASI_THICK, QUASI_INV, theta=theta)
        byp = UnloadedHole(bypass_correction, DIAMETER, QUASI_THICK, QUASI_INV)
        x, y = self.analysis.xy_points(rc=0., num=100)
        byp_stress = byp.stress(x, y)
        brg_stress = brg.stress(x, y)
        total_stress = byp_stress + brg_stress
        analysis_stress = self.analysis.stresses(bearing,
                                                 bypass,
                                                 rc=0.,
                                                 num=100,
                                                 w=w)
        assert_array_almost_equal(total_stress, analysis_stress)

    def test_max_strain(self):
        rc = 0.15
        num = 4
        bearing = [0, 0]
        bypass = [1000., 0., 0.]
        margins = self.analysis.analyze(bearing, bypass, rc=rc, num=num)
        strains = self.analysis.strains(bearing, bypass, rc=rc, num=num)
        compare_margins = np.empty((num, 2 * len(self.analysis.et)))
        with np.errstate(divide='ignore'):
            for iangle, angle in enumerate(self.analysis.et):
                rotated_strains = rotate_strains(strains,
                                                 angle=np.deg2rad(angle))
                # axial strains
                x_strains = rotated_strains[:, 0]
                compare_margins[:, iangle * 2] = np.select(
                    [x_strains > 0, x_strains < 0], [
                        QUASI_UNT / x_strains - 1,
                        -abs(QUASI_UNC) / x_strains - 1
                    ])
                # shear strains
                xy_strains = np.abs(rotated_strains[:, 2])
                compare_margins[:, iangle * 2 +
                                1] = abs(SHEAR_STRN) / xy_strains - 1
        assert_array_almost_equal(margins, compare_margins)

    def test_random_allowables(self):
        rc = 0.15
        num = 4
        bearing = [0, 0]
        bypass = [1000., 0., 0.]
        analysis = MaxStrain(QUASI,
                             QUASI_THICK,
                             DIAMETER,
                             et={0: QUASI_UNT},
                             ec={90: QUASI_UNC})
        margins = analysis.analyze(bearing, bypass, rc=rc, num=num)
        strains = analysis.strains(bearing, bypass, rc=rc, num=num)
        compare_margins = np.empty((num, 4))
        with np.errstate(divide='ignore'):
            # axial strains
            x_strains = strains[:, 0]
            compare_margins[:, 0] = np.select(
                [x_strains > 0, x_strains < 0],
                [QUASI_UNT / x_strains - 1, -np.inf / x_strains - 1])
            # shear strains
            xy_strains = np.abs(strains[:, 2])
            compare_margins[:, 1] = np.inf / xy_strains - 1
            rotated_strains = rotate_strains(strains, angle=np.deg2rad(90))
            # axial strains
            x_strains = rotated_strains[:, 0]
            compare_margins[:, 2] = np.select(
                [x_strains > 0, x_strains < 0],
                [np.inf / x_strains - 1, -abs(QUASI_UNC) / x_strains - 1])
            # shear strains
            xy_strains = np.abs(rotated_strains[:, 2])
            compare_margins[:, 3] = np.inf / xy_strains - 1
        assert_array_almost_equal(margins, compare_margins)
コード例 #7
0
ファイル: __main__.py プロジェクト: BenjaminETaylor/bjsfm
if instructions:
    print(
        'Input far field stresses, off-axis angle, bearing stress and bolt loading angle [Px, Py, Pxy, alpha, Pbr, theta]'
    )
px, py, pxy, alpha, pbr, theta = list(map(float, input().split(',')))

if instructions:
    print('Input width (0.0 for infinte plate)')
width = float(input())

if instructions:
    print(
        'Input bolt diameter, number of output points, step increment and number of steps desired'
    )
diameter, num_pts, step, num_steps = list(map(float, input().split(',')))

if 5 in output:
    analysis = MaxStrain([[a11, a12, a16], [a12, a22, a26], [a16, a26, a66]],
                         thickness,
                         diameter,
                         et=dict(zip(angles, tension)),
                         ec=dict(zip(angles, compression)),
                         es=dict(zip(angles, shear)))
else:
    analysis = MaxStrain([[a11, a12, a16], [a12, a22, a26], [a16, a26, a66]],
                         thickness, diameter)


def output_streses():
    pass