*HEADING EXAMPLE PROBLEM: MODE 0 SPHERE USING ACINAX3 *PREPRINT,MODEL=YES,ECHO=YES,HISTORY=YES *NODE,NSET=INNER 1, 0., 1., 0., 0., 1., 0. 2, 0.104528, 0.994522, 0., 0.104528, 0.994522 3, 0.207912, 0.978148, 0., 0.207912, 0.978148 4, 0.309017, 0.951057, 0., 0.309017, 0.951057, 5, 0.406737, 0.913545, 0., 0.406737, 0.913545 6, 0.5, 0.866025, 0., 0.5 , 0.866025 7, 0.587785, 0.809017, 0., 0.587785, 0.809017 8, 0.669131, 0.743145, 0., 0.669131, 0.743145 9, 0.743145, 0.669131, 0., 0.743145, 0.669131 10, 0.809017, 0.587785, 0., 0.809017, 0.587785 11, 0.866025, 0.5, 0., 0.866025, 0.5 12, 0.913545, 0.406737, 0., 0.913545, 0.406737 13, 0.951057, 0.309017, 0., 0.951057, 0.309017 14, 0.978148, 0.207912, 0., 0.978148, 0.207912 15, 0.994522, 0.104528, 0., 0.994522, 0.104528 16, 1., 0.0, 0., 1. , 0.0, 17, 0.994522, -0.104528, 0., 0.994522, -0.104528 18, 0.978148, -0.207912, 0., 0.978148, -0.207912 19, 0.951057, -0.309017, 0., 0.951057, -0.309017 20, 0.913545, -0.406737, 0., 0.913545, -0.406737 21, 0.866025, -0.5, 0., 0.866025, -0.5 22, 0.809017, -0.587785, 0., 0.809017, -0.587785 23, 0.743145, -0.669131, 0., 0.743145, -0.669131 24, 0.669131, -0.743145, 0., 0.669131, -0.743145 25, 0.587785, -0.809017, 0., 0.587785, -0.809017 26, 0.5, -0.866025, 0., 0.5, -0.866025 27, 0.406737, -0.913545, 0., 0.406737, -0.913545 28, 0.309017, -0.951057, 0., 0.309017, -0.951057 29, 0.207912, -0.978148, 0., 0.207912, -0.978148 30, 0.104528, -0.994522, 0., 0.104528, -0.994522 31, 0., -1., 0., 0., -1., ** *ELEMENT, TYPE=ACINAX3,ELSET=EALL 1, 1,3,2 *ELGEN, ELSET=EALL 1,15,2,1 *ELEMENT,TYPE=ASI3A,ELSET=COUPLING 1001, 1,2,3 *ELGEN,ELSET=COUPLING 1001,15,2,1 ** ** FLUID MATERIAL PROPERTIES; ARTIFICIAL MEDIUM FOR CONVENIENCE ** USING RHO = 1, BULKMOD = (2*PI)^2, WE HAVE C = 2*PI AND K = F. ** *MATERIAL,NAME=AETHER *DENSITY 1.000000, *ACOUSTIC MEDIUM,BULK MODULUS 39.4784176, *SOLID SECTION,MATERIAL=AETHER,ELSET=EALL 1.0, 0.0,0.0,0.0 *INTERFACE,ELSET=COUPLING ** *NSET,NSET=QA_TEST 1, 11, 16, 21, 31, *TRANSFORM,NSET=INNER,TYPE=C 0.,0.,0., 0.,0.,1. *STEP *STEADY STATE DYNAMIC,DIRECT 00.01, 0.05, 0.1, 0.13, 0.16, 0.2, 0.3, 0.4, 0.5, 0.6, 0.7, 0.8, 0.9, 1.0, 1.1, 1.2, 1.3, 1.4, 1.5, 1.6, 1.7, 1.8, 1.9, 2.0, 2.3, 2.5, 3.0, 4.0, 5.0, 6.0, 7.0, 8.0, 9.0, 10.0, 12.0, 15.0, 20.0, ** ** SURFACE RADIAL ACCELERATION OF 1/(RHO C) MAGNITUDE ** *BOUNDARY,TYPE=VELOCITY INNER,1,1,0.159154943 INNER,2,2,0.0 *NODE PRINT,NSET=QA_TEST,FREQUENCY=10000 POR,v *NODE FILE,NSET=QA_TEST,FREQUENCY=10000 POR,v *OUTPUT,FIELD *NODE OUTPUT POR,v *OUTPUT,HISTORY *NODE OUTPUT,NSET=QA_TEST POR,v *END STEP *****************************