----------- SubDyn v1.03.x MultiMember Support Structure Input File ------------ OC4 'Jacket' SubStructure Input File. The grouted connection is simulated with an equivalent tubular beam of enhanced properties. RRD 10/15/2013 -------------------------- SIMULATION CONTROL --------------------------------- False Echo - Echo input data to ".SD.ech" (flag) "DEFAULT" SDdeltaT - Local Integration Step. If "default", the glue-code integration step will be used. 3 IntMethod - Integration Method [1/2/3/4 = RK4/AB4/ABM4/AM2]. True SttcSolve - Solve dynamics about static equilibrium point -------------------- FEA and CRAIG-BAMPTON PARAMETERS--------------------------- 3 FEMMod - FEM switch: element model in the FEM. [1= Euler-Bernoulli(E-B) ; 2=Tapered E-B (unavailable); 3= 2-node Timoshenko; 4= 2-node … 2 NDiv - Number of sub-elements per member True CBMod - [T/F] If True perform C-B reduction, else full FEM dofs will be retained. If True, select Nmodes to retain in C-B reduced system. 8 Nmodes - Number of internal modes to retain (ignored if CBMod=False). If Nmodes=0 --> Guyan Reduction. 1 JDampings - Damping Ratios for each retained mode (% of critical) If Nmodes>0, list Nmodes structural damping ratios for each retained mode …. ---- STRUCTURE JOINTS: joints connect structure members (~Hydrodyn Input File)--- 64 NJoints - Number of joints (-) JointID JointXss JointYss JointZss [Coordinates of Member joints in SS-Coordinate System] (-) (m) (m) (m) 1 6.00000 6.00000 -45.50000 2 6.00000 6.00000 -45.00000 3 5.96700 5.96700 -44.00100 4 5.93900 5.93900 -43.12700 5 5.33300 5.33300 -24.61400 6 -6.00000 6.00000 -45.50000 7 -6.00000 6.00000 -45.00000 8 -5.96700 5.96700 -44.00100 9 -5.93900 5.93900 -43.12700 10 -5.33300 5.33300 -24.61400 11 -6.00000 -6.00000 -45.50000 12 -6.00000 -6.00000 -45.00000 13 -5.96700 -5.96700 -44.00100 14 -5.93900 -5.93900 -43.12700 15 -5.33300 -5.33300 -24.61400 16 6.00000 -6.00000 -45.50000 17 6.00000 -6.00000 -45.00000 18 5.96700 -5.96700 -44.00100 19 5.93900 -5.93900 -43.12700 20 5.33300 -5.33300 -24.61400 21 4.82000 4.82000 -8.92200 22 4.38500 4.38500 4.37800 23 4.01600 4.01600 15.65100 24 4.00000 4.00000 16.15000 25 -4.82000 4.82000 -8.92200 26 -4.38500 4.38500 4.37800 27 -4.01600 4.01600 15.65100 28 -4.00000 4.00000 16.15000 29 -4.82000 -4.82000 -8.92200 30 -4.38500 -4.38500 4.37800 31 -4.01600 -4.01600 15.65100 32 -4.00000 -4.00000 16.15000 33 4.82000 -4.82000 -8.92200 34 4.38500 -4.38500 4.37800 35 4.01600 -4.01600 15.65100 36 4.00000 -4.00000 16.15000 37 5.62000 0.00000 -33.37300 38 -5.62000 0.00000 -33.37300 39 0.00000 5.62000 -33.37300 40 0.00000 -5.62000 -33.37300 41 5.06400 0.00000 -16.37100 42 -5.06400 0.00000 -16.37100 43 0.00000 5.06400 -16.37100 44 0.00000 -5.06400 -16.37100 45 4.59200 0.00000 -1.95800 46 -4.59200 0.00000 -1.95800 47 0.00000 4.59200 -1.95800 48 0.00000 -4.59200 -1.95800 49 4.19300 0.00000 10.26200 50 -4.19300 0.00000 10.26200 51 0.00000 4.19300 10.26200 52 0.00000 -4.19300 10.26200 53 4.00000 4.00000 20.15000 54 -4.00000 4.00000 20.15000 55 4.00000 -4.00000 20.15000 56 -4.00000 -4.00000 20.15000 57 6.00000 -6.00000 -49.50000 58 6.00000 6.00000 -49.50000 59 -6.00000 -6.00000 -49.50000 60 -6.00000 6.00000 -49.50000 61 6.00000 -6.00000 -50.00100 62 6.00000 6.00000 -50.00100 63 -6.00000 -6.00000 -50.00100 64 -6.00000 6.00000 -50.00100 ------------------- BASE REACTION JOINTS: 1/0 for Locked/Free DOF @ each Reaction Node --------------------- 4 NReact - Number of Joints with reaction forces; be sure to remove all rigid motion DOFs of the structure (else det([K])=[0]) RJointID RctTDXss RctTDYss RctTDZss RctRDXss RctRDYss RctRDZss SSIfile [Global Coordinate System] (-) (flag) (flag) (flag) (flag) (flag) (flag) (string) 61 1 1 1 1 1 1 "OC4_Jacket_SD_SSI.txt" 62 1 1 1 1 1 1 "OC4_Jacket_SD_SSI.txt" 63 1 1 1 1 1 1 "OC4_Jacket_SD_SSI.txt" 64 1 1 1 1 1 1 "OC4_Jacket_SD_SSI.txt" ------- INTERFACE JOINTS: 1/0 for Locked (to the TP)/Free DOF @each Interface Joint (only Locked-to-TP implemented thus far (=rigid TP)) --------- 8 NInterf - Number of interface joints locked to the Transition Piece (TP): be sure to remove all rigid motion dofs IJointID ItfTDXss ItfTDYss ItfTDZss ItfRDXss ItfRDYss ItfRDZss [Global Coordinate System] (-) (flag) (flag) (flag) (flag) (flag) (flag) 24 1 1 1 1 1 1 28 1 1 1 1 1 1 32 1 1 1 1 1 1 36 1 1 1 1 1 1 53 1 1 1 1 1 1 54 1 1 1 1 1 1 55 1 1 1 1 1 1 56 1 1 1 1 1 1 ----------------------------------- MEMBERS -------------------------------------- 112 NMembers - Number of frame members MemberID MJointID1 MJointID2 MPropSetID1 MPropSetID2 COSMID (-) (-) (-) (-) (-) (-) 1 1 2 2 2 2 2 3 2 2 3 3 4 2 2 4 4 5 2 2 5 6 7 2 2 6 7 8 2 2 7 8 9 2 2 8 9 10 2 2 9 11 12 2 2 10 12 13 2 2 11 13 14 2 2 12 14 15 2 2 13 16 17 2 2 14 17 18 2 2 15 18 19 2 2 16 19 20 2 2 17 5 21 3 3 18 21 22 3 3 19 22 23 3 3 20 23 24 3 3 21 10 25 3 3 22 25 26 3 3 23 26 27 3 3 24 27 28 3 3 25 15 29 3 3 26 29 30 3 3 27 30 31 3 3 28 31 32 3 3 29 20 33 3 3 30 33 34 3 3 31 34 35 3 3 32 35 36 3 3 33 8 3 1 1 34 13 8 1 1 35 13 18 1 1 36 18 3 1 1 37 4 37 1 1 38 37 20 1 1 39 19 37 1 1 40 37 5 1 1 41 9 38 1 1 42 38 15 1 1 43 14 38 1 1 44 38 10 1 1 45 4 39 1 1 46 39 10 1 1 47 9 39 1 1 48 39 5 1 1 49 19 40 1 1 50 40 15 1 1 51 14 40 1 1 52 40 20 1 1 53 5 41 1 1 54 41 33 1 1 55 20 41 1 1 56 41 21 1 1 57 10 42 1 1 58 42 29 1 1 59 15 42 1 1 60 42 25 1 1 61 5 43 1 1 62 43 25 1 1 63 10 43 1 1 64 43 21 1 1 65 20 44 1 1 66 44 29 1 1 67 15 44 1 1 68 44 33 1 1 69 21 45 1 1 70 45 34 1 1 71 33 45 1 1 72 45 22 1 1 73 25 46 1 1 74 46 30 1 1 75 29 46 1 1 76 46 26 1 1 77 21 47 1 1 78 47 26 1 1 79 25 47 1 1 80 47 22 1 1 81 33 48 1 1 82 48 30 1 1 83 29 48 1 1 84 48 34 1 1 85 22 49 1 1 86 49 35 1 1 87 34 49 1 1 88 49 23 1 1 89 26 50 1 1 90 50 31 1 1 91 30 50 1 1 92 50 27 1 1 93 22 51 1 1 94 51 27 1 1 95 26 51 1 1 96 51 23 1 1 97 34 52 1 1 98 52 31 1 1 99 30 52 1 1 100 52 35 1 1 101 24 53 4 4 102 28 54 4 4 103 32 56 4 4 104 36 55 4 4 105 58 1 5 5 106 57 16 5 5 107 60 6 5 5 108 59 11 5 5 109 62 58 6 6 110 61 57 6 6 111 64 60 6 6 112 63 59 6 6 ------------------ MEMBER X-SECTION PROPERTY data 1/2 [isotropic material for now: use this table for circular-tubular elements] ------------------------ 6 NPropSets - Number of structurally unique x-sections (i.e. how many groups of X-sectional properties are utilized throughout all of the members) PropSetID YoungE ShearG MatDens XsecD XsecT (-) (N/m2) (N/m2) (kg/m3) (m) (m) 1 2.10000e+11 8.07690e+10 7850.00 0.800000 0.020000 2 2.10000e+11 8.07690e+10 7850.00 1.200000 0.050000 3 2.10000e+11 8.07690e+10 7850.00 1.200000 0.035000 4 2.10000e+11 8.07690e+10 7850.00 1.200000 0.040000 5 2.10000e+11 8.07690e+10 3339.12 2.082000 0.491000 6 2.10000e+11 8.07690e+10 7850.00 2.082000 0.060000 ------------------ MEMBER X-SECTION PROPERTY data 2/2 [isotropic material for now: use this table if any section other than circular, however provide COSM(i,j) below]- 0 NXPropSets - Number of structurally unique non-circular x-sections (if 0 the following table is ignored) PropSetID YoungE ShearG MatDens XsecA XsecAsx XsecAsy XsecJxx XsecJyy XsecJ0 (-) (N/m2) (N/m2) (kg/m3) (m2) (m2) (m2) (m4) (m4) (m4) ---------------------- MEMBER COSINE MATRICES COSM(i,j) ------------------------ 0 NCOSMs - Number of unique cosine matrices (i.e., of unique member alignments including principal axis rotations); ignored if NXPropSets=0 … COSMID COSM11 COSM12 COSM13 COSM21 COSM22 COSM23 COSM31 COSM32 COSM33 (-) (-) (-) (-) (-) (-) (-) (-) (-) (-) ------------------------ JOINT ADDITIONAL CONCENTRATED MASSES-------------------------- 0 NCmass - Number of joints with concentrated masses; Global Coordinate System CMJointID JMass JMXX JMYY JMZZ (-) (kg) (kg*m^2) (kg*m^2) (kg*m^2) ---------------------------- OUTPUT: SUMMARY & OUTFILE ------------------------------ True SDSum - Output a Summary File (flag).It contains: matrices K,M and C-B reduced M_BB, M-BM, K_BB, K_MM(OMG^2), PHI_R, PHI_L. IT can also … False OutCOSM - Output cosine matrices with the selected output member forces (flag) False OutAll - [T/F] Output all members' end forces 1 OutSwtch - [1/2/3] Output requested channels to: 1=.SD.out 2=.out (generated by FAST) 3=both files. True TabDelim - Generate a tab-delimited output in the .SD.out file 1 OutDec - Decimation of output in the .SD.out file "ES11.4e2" OutFmt - Output format for numerical results in the .SD.out file "A11" OutSFmt - Output format for header strings in the .SD.out file ------------------------- MEMBER OUTPUT LIST ------------------------------------------ 8 NMOutputs - Number of members whose forces/displacements/velocities/accelerations will be output (-) [Must be <= 9]. MemberID NOutCnt NodeCnt [NOutCnt=how many nodes to get output for [< 10]; NodeCnt are local ordinal numbers from the start of the member, and must be >=1 and … (-) (-) (-) 22 1 3 30 1 3 73 1 3 83 1 3 41 2 2 3 51 2 2 3 6 1 3 14 1 3 ------------------------- SDOutList: The next line(s) contains a list of output parameters that will be output in .SD.out or .out. ------ "M1N1FKZe, M2N1FKZe" - Axial force in leg 2 at K1L2 and in leg 4 at K1L4 "M3N1TDXss, M3N1TDYss, M3N1TDZss, M4N1TDXss, M4N1TDYss, M4N1TDZss" - Deflections at X2S2, X2S3: use cosdir matrix to get Out-of-plane (OOP) deflection "M5N2TDXss, M5N2TDYss, M5N2TDZss, M6N2TDXss, M6N2TDYss, M6N2TDZss" - Deflections at X4S2, X4S3: use cosdir matrix to get OOP deflection "M5N1FKXe,M5N1FKYe,M5N1FKZe,M6N1FKXe,M6N1FKYe,M6N1FKZe" - Forces OOP and Axial at mid brace points x,y, z >> *we will need to do some post-processing "M7N1FKZe, M8N1FKZe" - Axial force in leg 2 and leg 4 at mudbrace level: MudbraceL2, MudbraceL4 "-ReactFXss, -ReactFYss, -ReactMXss, -ReactMYss, -ReactMZss, -ReactFZss" - Base reactions: fore-aft shear, side-to-side shear, side-to-side moment, fore-aft moment, … END of output channels and end of file. (the word "END" must appear in the first 3 columns of this line)