*HEADING Cylindrical element testing under traction load(CCL18) *PREPRINT, ECHO=YES, MODEL=YES, HISTORY=YES ** ********************************************************** ** Parameter definition ** *PARAMETER INRAD=1.5 EXRAD=2.0 HEIGHT=1.0 ** MIDHEIGHT=HEIGHT/2 MID=(INRAD+EXRAD)/2 ** *********************************************************** ** Model definition ** *NODE, NSET=SECTION 1, ,0,0 2, ,0,0 3, ,0, 4, ,0, 5,,0,0 6,,0, 7,,0, 8,,0, 9,,0, *NCOPY, CHANGE NUMBER=100, OLD SET=SECTION, NEW SET=REST, SHIFT, MULTIPLE=7 0,0,0 0,0,0,0,0,1,45 *NSET, NSET=ALL REST,SECTION ** *NSET, NSET=INT, GENERATE 1,701,100 4,704,100 8,708,100 *NSET, NSET=EX, GENERATE 2,702,100 3,703,100 6,706,100 *NSET, NSET=TOP, GENERATE 3,703,100 4,704,100 7,707,100 *NSET, NSET=BOTTOM, GENERATE 1,701,100 2,702,100 5,705,100 *NSET, NSET=AR1, GENERATE 1,701,100 *NSET, NSET=AR2, GENERATE 2,702,100 *NSET, NSET=AR3, GENERATE 3,703,100 *NSET, NSET=AR4, GENERATE 4,704,100 ** *ELEMENT, TYPE=CCL18, ELSET=LAST 7, 1,2,3,601,602,603,701,702,703,5,6,9,605,606,609,705,706,709 8, 1,3,4,601,603,604,701,703,704,9,7,8,609,607,608,709,707,708 *ELEMENT, TYPE=CCL18, ELSET=FIRST 1, 201,202,203,1,2,3,101,102,103,205,206,209,5,6,9,105,106,109 2, 201,203,204,1,3,4,101,103,104,209,207,208,9,7,8,109,107,108 *ELGEN, ELSET=FIRST3 1,3,200,2 2,3,200,2 *ELSET, ELSET=ALL FIRST3,LAST *SOLID SECTION, ELSET=ALL, MATERIAL=MYMAT *MATERIAL, NAME=MYMAT *ELASTIC 30E6,0.3 ************************************************************ ** Boundary Condition *TRANSFORM, TYPE=C, NSET=ALL 0,0,0, 0,0,1 *ORIENTATION, SYSTEM=C, NAME=CYL 0,0,0, 0,0,1 *BOUNDARY INT,1,3,0 ************************************************************ ** History data ** *STEP, NLGEOM=YES, UNSYMM=YES *STATIC 0.1,1.0 *DLOAD,orientation=cyl 1,TRVEC4,-5e6,0,1,0 3,TRVEC4,-5e6,0,1,0 5,TRVEC4,-5e6,0,1,0 7,TRVEC4,-5e6,0,1,0 *OUTPUT, FIELD *NODE OUTPUT, VARIABLE=PRESELECT *END STEP