ESD.77 Multidisciplinary System Design Optimization Spring Barge Design Optimization
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1 ESD.77 Multidisciplinary System Design Optimization Spring 2010 Barge Design Optimization Anonymous MIT Students
2 What is a barge? Flat bottomed vessel, typically non selfpropelled, used to carry low value, heavy or bulky items. 2
3 Motivation Interest in marine environment disciplines. Opportunity to use and bring together previous academic experience. A common ship design problem would be extremely complex to handle in one semester. 3
4 Multi disciplinary ESD.77 M φ WL Hydrostatics Image by MIT OpenCourseWare. WL" WL φ Z G B W N K e Ship Motion Degrees of Freedom Heave WL" Yaw Hydrodynamics Surge Roll Pitch Image by MIT OpenCourseWare. Structural Mechanics Sway Compressive stress in deck 4 Tensile stress in keel Image by MIT OpenCourseWare.
5 Problem Formulation Design Variables Lower Bound Upper Bound Unit L Length m B Beam m D Depth 4 9 m t Plate Thickness mm Design Parameters Value Unit v Speed 10 knots kg Payload vertical center of gravity 1.2D lcg Payload longitudinal center of gravity 0.5L ω Peak spectral frequency 0.7 rad/sec H Significant wave height 2.5 m ρ Sea water density 1025 kg/m 3 ρ str Material thickness 7850 kg/m 3 Design Objective is to maximize payload (P) s.t. Inequality Constraints N<60 Number of occurences of green water on deck per hour T<6m Draft GM>0.15m Metacentric height σ k,sag <250MPa Keel stress at sagging wave σ k,hog <250MPa Keel stress at hogging wave σ d,sag <250MPa Deck stress at sagging wave σ d,hog <250MPa Deck stress at hogging wave Barge cross section 5
6 Input/Output Diagram v Hydrodynamics N Inputs T Outputs L,B,D,t Hydrosta atics GM P,w str Structural Mechanics σ max May 5,2010 6
7 Modeling in MATLAB Multidisciplinary Feasible (MDF) Model Payload, the objective function, is also required as input by all modules. Feasibility is enforced at each optimization iteration. May 5,2010 7
8 Modeling in MATLAB ESD.77 Hydrodynamics Curve fitting of experimental local hydrodynamics properties from Lewis theory to allow for a continuous design space exploration. Seakeeping analysis for coupled heave and pitch motions using 2D strip theory. Surge Ship Motion Degrees of Freedom Heave Yaw Pitch Roll Sway Image by MIT OpenCourseWare. Assumption: Bretschneider spectrum with significant wave height of 2.5m and peak spectral frequency of 0.7rad/sec 8
9 Modeling in MATLAB ESD.77 Hydrostatics Determines the vertical metacentric height which is evaluated against American Bureau of Shipping (ABS) rules. WL" WL M φ φ Z G B W N K e WL WL" Image by MIT OpenCourseWare. Assumption: Vertical position of payload s center of gravity at 1.2*D 9
10 Modeling in MATLAB ESD.77 Structural Mechanics Uses ABS parametric equations to determine maximum keel and deck stresses in sagging and hogging wave conditions. Compressive stress in deck Assumptions: Uniform longitudinal weight distribution. Tensile stress in keel Image by MIT OpenCourseWare. 10
11 Simulation and Benchmarking L 122 P=14,670tons B 30 T=4.35m D 6.1 N is the active constraint x = = t 16 Source: McDonough Marine Service 11
12 Initial Design Space Exploration ESD.77 4 Design variables 3 Level (lower bound, mid, higher bound) JMP Statistical Software Generate DOE to capture main effect and two way interactions 48 runs (16 were unfeasible) 12
13 Initial Design Space Exploration Analysis of 32 feasible designs: ESD.77 Recommended starting point for numerical optimization: 140 x =
14 Gradient Based Optimization SQP MATLAB s fmincon : Ability to handle multiple variables Ability to handle design variables bounds Results: P=23,530tons: * x = 34.2 vs. x =
15 Sensitivity Analysis Variables: t Normalized Sensitivities Design Variable D B L Parameters: Normalized Sensitivities H Active constraints: Parameter Design ω kg v N σ d,hog 15
16 Post Optimality Analysis Hessian diagonal entries close to O(1) No improvement was achieved by trying to scale the design variables -2 x 104 Current Function Value: Function value Iteration 16
17 Heuristic Optimization Genetic Algorithm: Easy implementation of fitness function Close to the optimum Results: P=22,468tons at x = 34.6 vs. x * =
18 Global Optimum Leveraging: DOE Gradient based optimization GA Maximum Payload of P=23,530tons at x * =
19 Multi Objective Optimization Optimal Point Utopia Point Trade off analysis at optimal payload solution: For an extra ton of payload we need to add 244kg of structural weight 19
20 Conclusions Model fidelity can be improved: Cross section, scantlings, non uniform plate thickness Consider most appropriate sea spectrum Evaluate all 6 degree of freedom motions and most importantly roll. But will make optimization more challenging. 20
21 Back up 21
22 MIT OpenCourseWare ESD.77 / Multidisciplinary System Design Optimization Spring 2010 For information about citing these materials or our Terms of Use, visit:
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