예제 #1
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 def test_memb_maxstrain(self):
     plainstrength.failure_analysis_c(self.mlam, self.load3, self.dtemp,
                                      'MaxStrain')
예제 #2
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 def test_memb_airbus(self):
     plainstrength.failure_analysis_c(self.mlam, self.load3, self.dtemp,
                                      'Airbus')
예제 #3
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 def test_memb_modpuck(self):
     plainstrength.failure_analysis_c(self.mlam, self.load3, self.dtemp,
                                      'ModPuck')
예제 #4
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 def test_memb_puckC(self):
     plainstrength.failure_analysis_c(self.mlam, self.load3, self.dtemp,
                                      'Puck C')
예제 #5
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 def test_memb_hashina(self):
     plainstrength.failure_analysis_c(self.mlam, self.load3, self.dtemp,
                                      'Hashin A')
예제 #6
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 def test_memb_hashinb(self):
     r, hist = plainstrength.failure_analysis_c(self.mlam, self.load3,
                                                self.dtemp, 'Hashin B')
     print(r, hist)
예제 #7
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 def test_flex_airbus(self):
     plainstrength.failure_analysis_c(self.lam, self.load6, self.dtemp,
                                      'Airbus')
예제 #8
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 def test_flex_maxstrain(self):
     plainstrength.failure_analysis_c(self.lam, self.load6, self.dtemp,
                                      'MaxStrain')
예제 #9
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 def test_flex_puckC(self):
     plainstrength.failure_analysis_c(self.lam, self.load6, self.dtemp,
                                      'Puck C')
예제 #10
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 def test_flex_modpuck(self):
     plainstrength.failure_analysis_c(self.lam, self.load6, self.dtemp,
                                      'ModPuck')
예제 #11
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 def test_flex_hashinb(self):
     plainstrength.failure_analysis_c(self.lam, self.load6, self.dtemp,
                                      'Hashin B')