📄 spacetrusselementstiffness.m
字号:
function y = SpaceTrussElementStiffness(E,A,L,thetax,thetay,thetaz)
%SpaceTrussElementStiffness This function returns the element
% stiffness matrix for a space truss
% element with modulus of elasticity E,
% cross-sectional area A, length L, and
% angles thetax, thetay, thetaz
% (in degrees). The size of the element
% stiffness matrix is 6 x 6.
x = thetax*pi/180;
u = thetay*pi/180;
v = thetaz*pi/180;
Cx = cos(x);
Cy = cos(u);
Cz = cos(v);
w = [Cx*Cx Cx*Cy Cx*Cz ; Cy*Cx Cy*Cy Cy*Cz ; Cz*Cx Cz*Cy Cz*Cz];
y = E*A/L*[w -w ; -w w];
⌨️ 快捷键说明
复制代码
Ctrl + C
搜索代码
Ctrl + F
全屏模式
F11
切换主题
Ctrl + Shift + D
显示快捷键
?
增大字号
Ctrl + =
减小字号
Ctrl + -