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com:nastranfrom [2018/02/20 09:32]
phil
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-====== CTR Command Transformations ====== 
  
-The transformation equations for the [[com:​CTRVEC]] and [[com:​CTRCCV]] commands. ​   ​ 
- 
-===== Stress Transformation Equations ===== 
- 
-#;; 
-\(\quad \alpha = \text{Angle between global X and local X}\)\\ 
-\(\quad t = \text{Shell thickness}\)\\ 
-\(\quad E = \text{Shell material Young'​s modulus}\)\\ 
-\(\quad \nu = \text{Shell material Poisson ratio}\)\\ 
-#;; 
-==== Thin Shell ==== 
-#;; 
-\( \quad S_{x_G} = S_{x_L}*cos^2(\alpha)+2*S_{xy_L}*sin(\alpha)*cos(\alpha)+S_{y_L}sin^2(\alpha) \) 
-\( \quad S_{y_G} = S_{x_L}*sin^2(\alpha)-2*S_{xy_L}*sin(\alpha)*cos(\alpha)+S_{y_L}cos^2(\alpha) \) 
-\( \quad S_{xy_G} = S_{xy_L}*(cos^2(\alpha)-sin^2(\alpha))-(S_{y_L}+S_{x_L})*sin(\alpha)*cos(\alpha) \) 
-\( \quad M_{x_G} = M_{x_L}*cos^2(\alpha)+2*M_{xy_L}*sin(\alpha)*cos(\alpha)+M_{y_L}sin^2(\alpha) \) 
-\( \quad M_{y_G} = M_{x_L}*sin^2(\alpha)-2*M_{xy_L}*sin(\alpha)*cos(\alpha)+M_{y_L}cos^2(\alpha) \) 
-\( \quad M_{xy_G} = M_{xy_L}*(cos^2(\alpha)-sin^2(\alpha))-(M_{y_L}+M_{x_L})*sin(\alpha)*cos(\alpha) \) 
-#;; 
-==== Thick  Shell ==== 
-\( \quad N_{x_G} = N_{x_L}*cos^2(\alpha)+2*N_{xy_L}*sin(\alpha)*cos(\alpha)+N_{y_L}sin^2(\alpha) \) 
-\( \quad N_{y_G} = N_{x_L}*sin^2(\alpha)-2*N_{xy_L}*sin(\alpha)*cos(\alpha)+N_{y_L}cos^2(\alpha) \) 
-\( \quad N_{xy_G} = N_{xy_L}*(cos^2(\alpha)-sin^2(\alpha))-(N_{y_L}+N_{x_L})*sin(\alpha)*cos(\alpha) \) 
-\( \quad M_{x_G} = M_{x_L}*cos^2(\alpha)+2*M_{xy_L}*sin(\alpha)*cos(\alpha)+M_{y_L}sin^2(\alpha) \) 
-\( \quad M_{y_G} = M_{x_L}*sin^2(\alpha)-2*M_{xy_L}*sin(\alpha)*cos(\alpha)+M_{y_L}cos^2(\alpha) \) 
-\( \quad M_{xy_G} = M_{xy_L}*(cos^2(\alpha)-sin^2(\alpha))-(M_{y_L}+M_{x_L})*sin(\alpha)*cos(\alpha) \) 
-\( \quad Q_{x_G} = Q_{x_L}*cos(\alpha)+Q_{y_L}*sin(\alpha) \) \\ 
-\( \quad Q_{y_G} = -Q_{x_L}*sin(\alpha)+Q_{y_L}*cos(\alpha) \) 
-===== Strain ​ Equations ===== 
-$$ \varepsilon_x = \frac{\sigma_x}{E}-\nu \frac{\sigma_y}{E} \qquad \varepsilon_y = \frac{\sigma_y}{E}-\nu \frac{\sigma_x}{E} \qquad \varepsilon_{xy} = \frac{\tau_{xy}}{E}*2(1+\nu) ​ $$ 
-$$\varepsilon_{1,​2} = \frac{\varepsilon_x+\varepsilon_y}{2} \pm \frac{\sqrt{(\varepsilon_x-\varepsilon_y)^2+\varepsilon_{xy}^2}}{2}$$ 
-==== Thin Shell ==== 
-$$ \sigma_x=S_{x_G} \pm \frac{6*M_{x_G}}{t^2} \qquad \sigma_y=S_{y_G} \pm \frac{6*M_{y_G}}{t^2} \qquad \tau_{xy}=S_{xy_G} \pm \frac{6*M_{xy_G}}{t^2}$$ 
- 
-==== Thick  Shell ==== 
-$$ \sigma_x=\frac{N_{x_G}}{t} \pm \frac{6*M_{x_G}}{t^2} \qquad \sigma_y=\frac{N_{y_G}}{t} \pm \frac{6*M_{y_G}}{t^2} \qquad \tau_{xy}=\frac{N_{xy_G}}{t} \pm \frac{6*M_{xy_G}}{t^2}$$ 
com/nastranfrom.1519137121.txt.gz ยท Last modified: 2018/02/20 09:32 by phil