$ TEST No IC18 - HEMISPHERE WITH POINT LOADS $ $ Short description: $ The system is generated in such a manner, so as to allow the calculation of $ several different element meshes consisting of quad-elements. The following $ element meshes are investigated: 4x4 elements (mesh partitioning 2), $ 8x8 elements (mesh partitioning 4) and 16x16 elements (mesh partitioning 8). $ The calculation is made with the program ASE. $ $ Results: $ - Comparative value x-displacement in point A: Desired value 0.185 m analytical, $ 0.1838 m fine mesh (8x8) 8-node quad-element $ values obtained with ASE: $ 4x4: 0.12006 m $ 8x8: 0.17978 m $ 16x16: 0.18492 m $ $ further results of the ASE-calculation: values in m $ Displacements $ $ Point A = Point 1 Point B = Point 9 Point C $ Vx Vz Vx Vy Vz Vy $ -------------------------------------------------------------------- $ 4x4 0.12006 0.06356 0.03953 -0.03953 0.0 -0.12006 $ 8x8 0.17978 0.08965 0.06036 -0.06036 0.0 -0.17978 $ 16x16 0.18492 0.09069 0.06244 -0.06244 0.0 -0.18492 $ $ Theory 0.185 -0.185 $ $ Bench- $ mark 0.1838 Print error 0.0628 -0.0628 0.0 $ round 0.09 $ $ Note print error in the result lists: false Vz in point 1 0. $ correct Vz in point 1 round 0.09 m $ (see also boundary conditions) PROG GENF urs:4 HEAD TEST No IC18 - HEMISPHERE WITH POINT LOADS TXB Element mesh with 2,4,8 elements symmetric about point G SYST SPAC MAT 1 E 68.25e6 MUE 0.3 GRP 0 T 0.04 $ LET#4 8 $ mesh partitioning (<9!), only 1,2,4,8 are possible LET#9 10. $ Radius $ $ DEFINE ALL ELEMENTS WITH A CUBE NODE 101 #9 0 0 109 #9 #9 0 909 0 #9 0 181 #9 0 #9 189 #9 #9 #9 981 0 0 #9 989 0 #9 #9 MESH 101 109 189 181 #4 #4 MNO 1 181 189 989 981 #4 #4 MNO 1 109 909 989 189 #4 #4 MNO 1 $ NODE (101 181 (181-101)/#4) FIX PYYM ; (181 981 (981-181)/#4) == (909 989 (989-909)/#4) FIX PXXM ; (981 989 (989-981)/#4) == 981 FIX F $ 101,909,981 FIX XPYM,YPXM,F $ $ $BLOCK BEG1 $ SUB-PROGRAM FOR NODE GENERATION IN A COORDINATE THIRD $ NODE COORDINATES WITH NONLINEAR INCREMENT ROTATION $ #1,#2,#3 = NODE NUMBER ON AXIS + INCREMENTS LET#10 0,45/#4 $ initial value + increment phi-Y LOOP #4+1 LET#20 0,45/#4 $ initial value + increment phi-Z LOOP #4+1 LET#90 SQR(TAN(#10)**2+TAN(#20)**2) LET#91 ATN(#90) LET#92 COS(#91),0.0 LOOP #91-0.001 ; LET#93 SIN(#91)/#90 ; ENDLOOP -1 $ knoten: #1 #9*#92 #9*TAN(#20)*#93 #9*TAN(#10)*#93 $ LET#20 #20+#21 LET#1 #1+#3 ENDLOOP LET#10 #10+#11 LET#1 #1-#3*(#4+1)+#2 ENDLOOP $BLOCK END1 $ LET#1 101,(181-101)/#4,(109-101)/#4 $ node number + increments of X-sector NODE NO X Y Z $BLOCK SET1 $ LET#1 909,(109-909)/#4,(989-909)/#4 $ node number + increments of Y-sector NODE NO Y Z X $BLOCK SET1 $ LET#1 981,(989-981)/#4,(181-981)/#4 $ node number + increments of Z-sector NODE NO Z X Y $BLOCK SET1 $ END PROG ASE urs:5 HEAD TEST No IC18 - HEMISPHERE WITH POINT LOADS TXB Element mesh with 2,4,8 elements symmetric about point G ECHO ERIN AUS LC 1 LOAD 101 PX 2. LOAD 909 PY -2. END PROG WING urs:3 SIZE LP 0 VIEW STAN 1 1 1 NEGZ STRU 1 1 LOAD FULL COLO C5 6001 6001 6001 6001 ; DEFO 1 10.0 ; STRU 0 0 ; AND COLO C5 1002 1002 1002 1002 ; DEFO 0 ; STRU 0 0 NODE UX UNIT 1000 SCHH 0.1 ND 4 NODE UY UNIT 1000 SCHH 0.1 ND 4 NODE UZ UNIT 1000 SCHH 0.1 ND 4 NODE U UNIT 1000 SCHH 0.1 ND 4 QUAD SXM SCHH 0.1 STYP NODE QUAD SYM SCHH 0.1 STYP NODE END END