Stiffened Composite Panel Design

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Stiffened Composite Panel Design • Based on “Improved genetic algorithm for the design of stiffened composite panels,” by Nagendra, Jestin, Gurdal, Haftka, and Watson, Computers and Structures, pp. 543-555, 1996. • Standard genetic algorithm did not work well enough even with simplified structural model (finite strip). • Algorithm was improved based on simplified version of the panel design problem (e.g. fixed blade height, single laminate).

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Stiffened Composite Panel Design. Based on “Improved genetic algorithm for the design of stiffened composite panels,” by Nagendra , Jestin , Gurdal, Haftka , and Watson, Computers and Structures, pp. 543-555, 1996. - PowerPoint PPT Presentation

Transcript of Stiffened Composite Panel Design

Page 1: Stiffened Composite Panel Design

Stiffened Composite Panel Design

• Based on “Improved genetic algorithm for the design of stiffened composite panels,” by Nagendra, Jestin, Gurdal, Haftka, and Watson, Computers and Structures, pp. 543-555, 1996.

• Standard genetic algorithm did not work well enough even with simplified structural model (finite strip).

• Algorithm was improved based on simplified version of the panel design problem (e.g. fixed blade height, single laminate).

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Geometry and loading

20,000 /5,000 /

x

xy

N lb inN lb in

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Modeling in PASCO• Finite strip model assume that in one direction we

can use sine solution, while in the other the displacement can have general shape.

• Panel Analysis and sizing code (Stroud and Anderson) based on analysis code by Wittrick and Williams.

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Optimization problem

• Minimize the weight of the panel

• Design variables ply angles of skin (), ply angles of blade ()and flange (same), blade height.

• Outer plies limited tofor damage tolerance.• Constraints: Buckling load multiplier, strain-failure

load multiplier, balanced laminates, no more than four contiguous plies of same orientation.

2 2

4 2

960 , 30 , 72

s s b b b f

s b b f

W t n A n A n A

A in A H A in

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Optimization formulation

• Constrained version• Plies in stacks of two.• Unconstrained version

• Contiguity violation: Number of contiguous zero or ninety stacks in excess of 2 (for example 2 for

,( , , )

11

0

i bb b sH

b

s

Minimize W H n n

Suchthat

g

2

2

1

1

min ,

cont failfail

fail cont fail

fail b s

W PF

W P

110

sk blcont

nv nvP

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Material properties

• Today’s graphite-epoxys can do much better.

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Genetic code

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Selection and Crossover

• Rank based fitness and roulette wheel selection.• Original crossover is a 2-point crossover applied

to entire genome.• Two children produced.• Improved crossover applied individually to each

of the three substrings.• Crossover applied with 95% probability. If not,

first parent copied into next generation.

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Mutations• Mutation applied to one child with each gene mutated

with 3% probability to random new gene.• Improved mutation separates orientation mutations from

deletion and addition mutations.• Stack deletion: First select randomly skin or blade. Then

stack closest to mid-plane deleted with Probability of 2-3%.• Stack addition: Skin or blade selected randomly, then

random stack added at mid-plane.• New: Permutation, intra-laminar swap, inter-laminar swap.

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Results with original GA

• What is the main difference between rounded continuous optimum and GA design?

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Tuning the algorithm

• Probabilities associated with the different operators tuned on a simplified problem.

• For simplified problem, the blade laminate and blade height was fixed based on previous results.

• This reduced number of designs from to

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Improved GA designs

• What is different?

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Comparison