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案例(AUTODYN):射流形成、拉伸、映射及侵蚀靶板

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(1)射流形成和拉伸

 Part 1 –Axial 2D Shaped Charge Jet Formation

• New Model

– Ident: 2DShaped

– Symmetry: 2D and Axial

• Define Materials

• Load AL2024T351 (Shock –JC), Copper (Shock –none) and TNT.

• Modify AL2024T351

– Add failure to the model (plastic strain of 25%)

– Add erosion to the model: instantaneous geometric strain at 250%.

• Modify TNT

– Under cutoffs, change the minimum density factor to 1.e-6.

• Create a New Material

– Name = air

–EOS is ideal gas: r ref = 1.225e-3, γ = 1.4, Tref = 288, cv = 717.5



• Define Initial Conditions

– Name =StillAir.

– Material = air

– Internal Energy = 206640 J.

• Define Boundary Conditions

– Name = FlowOut,

– Type =Euler flowout.

• Define Part

– Name = Space

– Solver = Euler

– Select Part Wizard

– Select Box: X origin = -100, Y origin = 0.0, DX = 275, and DY = 100

– Define cells in I = 550, Cells in J = 200

– Grade zoning in I, 225*0.25 mm, centred

– Grade zoning in J, 100*0.25 mm, lower J.

– Fill with initial condition: StillAir



• Fill Euler Part

– Rectangle

• x1,x2,y1,y2 = -50, -3, 0, 20

• Fill inside with TNT

– Quad

• Points = (-3,10), (84,43), (-20,43), (-50,20)

• Fill inside with TNT

– Ellipse

• X centre = 0, Y centre = 0.0, X semi-axis = Y semi-axis = 10

• Fill Inside with initial conditionStillAir

• Import from TrueGrid

– Open liner.zon

– Import the part LINER as Lagrange

– Fill part with Copper

• Part Fill LINER into the Euler part

– Select the subgrid LINER and the material TNT to replace.

– Repeat this, but select the material AIR to be replace.

• Delete the part LINER

• Define Boundary Conditions

– I line, I = 1, J = 1, 201, boundary: Flowout

– J line, I = 1, 501, J = 201, boundary: Flowout


•load from part library casing.slb


• Define Lagrange/Lagrange Interactions

– Gap size = 0.2

• Define Euler/Lagrange Interactions

– Select Automatic (polygon free)

• Define Detonation

– Press Line

–Point 1 = (-4.95E+01, 0.00E+00)

–Point 2 = (-4.95E+01, 1.00E+01)

– Initiation time = 0.00E+00

– Range of Influence = Unrestricted

• Define Wrapup Criteria (Controls)

– Cycle Limit = 10000, Time Limit = 0.04, Energy fraction = 0.05

• Define Save Times (Output)

• Start time = 0, End time = 10000, Increment = 0.001

• Save and Execute



 Part 2 –Rezoning the Euler Mesh and Continuation of Jetting

• Open Model of the previous simulation at time 40μs(cycle 2619)

• Delete Part Casing

• Modify Euler part IJK Range

– New I range = 101-651

– New J range = 1-133

• Manual Zoning (Euler Part)

– Define Node

• I = 551, J = 1, X = 342.0 , Y = 0.0

– Define Line

• IJK range: I = 451,551 J = 1,133

• I varies, J index = 1, Geom. ratio = 1.0

– Define Surface

• IJK range: I = 451,551 J = 1,133


 

• Fill Block

–I = 451, 551 J = 1, 133

– With initial condition StillAir

• Define Wrapup Criteria (Controls)

• Cycle Limit = 10000

• Time Limit = 0.06

• Energy fraction = 0.05

• Save and Execute.


(2)射流映射和侵彻靶板






来源:浅香岁月
ACTAutodynUMTrueGridOrigin
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首次发布时间:2025-12-10
最近编辑:10月前
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硕士 | 高级仿真应用... 显式动力学
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