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Structural Design and Response in Collision and Grounding

Structural Design and Response in Collision and Grounding

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ybeg<strong>in</strong>n<strong>in</strong>g of time step nStrik<strong>in</strong>g ShipP 4,n+1, P5,n+1 P1,n P1,n+1G 2Strik<strong>in</strong>g ShipG 1θ2φξP4,n, P5,nend of time step nφ ′ nP3,nαP2,nP2,n+1side shellStruck Shiplθ1Struck ShipP3,n+1damaged area dur<strong>in</strong>gtime step nNote: The positive direction of angle is alwayscounterclockwise.xFigure 14. Sweep<strong>in</strong>g Segment MethodηFigure 13. SIMCOL External Ship DynamicsV.U. M<strong>in</strong>orsky conducted the first <strong>and</strong> best known ofthe empirical collision studies based on actual data [26].His method relates the energy dissipated <strong>in</strong> a collisionevent to the volume of damaged structure. Actualcollisions <strong>in</strong> which ship speeds, collision angle, <strong>and</strong>extents of damage are known were used to empiricallydeterm<strong>in</strong>e a l<strong>in</strong>ear constant. This constant relates damagevolume to energy dissipation. In the orig<strong>in</strong>al analysis thecollision is assumed to be totally <strong>in</strong>elastic, <strong>and</strong> motion islimited to a s<strong>in</strong>gle degree of freedom. Under theseassumptions, a closed form solution for damaged volumecan be obta<strong>in</strong>ed. With additional degrees of freedom, atime-stepped solution must be used.Crake <strong>and</strong> Brown developed SIMCOL Version 0.0 aspart of the work of SNAME Ad Hoc Panel #3 [6,28].Based on further research, test runs <strong>and</strong> the need to makethe model sensitive to a broader range of design <strong>and</strong>scenario variables, improvements were progressivelymade by Chen <strong>and</strong> Brown at Virg<strong>in</strong>ia Tech [22]. Asweep<strong>in</strong>g segment method, shown <strong>in</strong> Figure 14, is addedto the model <strong>in</strong> SIMCOL Version 1.0 to improve thecalculation of damage volume <strong>and</strong> the direction ofdamage forces. Models from the Rosenblatt study [24,25]are applied <strong>in</strong> Version 1.1 assum<strong>in</strong>g rigid web frames. InVersion 2.0, the lateral deformation of web frames is<strong>in</strong>cluded as shown <strong>in</strong> Figure 15. In Version 2.1, thevertical extent of the strik<strong>in</strong>g ship bow is considered.Table 1 describes the evolution of SIMCOL over thecourse of the study thus far.<strong>Design</strong> data required for the strik<strong>in</strong>g ship <strong>in</strong>cludesbow half-entrance angle, bow height, length, beam, draft<strong>and</strong> displacement.Scenario data required <strong>in</strong>cludes strik<strong>in</strong>g <strong>and</strong> struckship velocity, collision angle, <strong>and</strong> longitud<strong>in</strong>al location ofimpact <strong>in</strong> the struck ship.Web frames act<strong>in</strong>g as a vertical beamdistort <strong>in</strong> bend<strong>in</strong>g, shear or compressionStrike at webframeAnalyze each shellseparatelyconsistent withweb deformation.Strike betweenweb frameAnalyze each shellseparately withnodes consistentwith webdeformation.Figure 15. Web Deformation <strong>in</strong> SIMCOL 2.0 [24,25]5.2.2 DAMAGE 4.0 [19]The DAMAGE 4.0 collision module solves the externalproblem uncoupled from the <strong>in</strong>ternal problem, <strong>and</strong> appliesthe calculated absorbed energy to plastic deformation ofthe struck ship. <strong>Structural</strong> components, motions, massesetc. are described <strong>in</strong> ship coord<strong>in</strong>ate systems local to eachship <strong>and</strong> <strong>in</strong> one global coord<strong>in</strong>ate system. Degrees offreedom <strong>in</strong> DAMAGE <strong>in</strong>clude strik<strong>in</strong>g ship surge <strong>and</strong>struck ship sway <strong>and</strong> yaw.The follow<strong>in</strong>g assumptions are applied <strong>in</strong> DAMAGE4.0:• Both ships are perpendicular before <strong>and</strong> dur<strong>in</strong>gimpact, i.e. only right angle collisions are considered.• The forward motion of the struck ship is assumed tobe zero.9

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