2006 Workshop LEEDS

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    1 FLACS 2006

    FLACS TRAINING EXERCISES

    Exercise I (and III): Explosion simulation in offshore platform moduleExplosion tests in an offshore test geometry will be simulated. A step by stepdescription will be available to give a flying start in the explosion modelling.

    Exercise II: Geometry building, designing Bang-box and explode

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    Exercise Ia: Explosion simulation in offshore module

    Typing convention: Command Explanation

    To be typed in unix-shells (boldface): cd TEST_EXAMPLE ( means Carriage return)

    To be typed in CASD command line (italic): vi 3 abbreviated VIEW menu, 3D View

    Keyboard shortcuts in CASD or FLOWVIS (underline): ALT-v 3 same effect as above in CASD

    To be typed by mouse or in dialog window (boldface) 3 4 enter 3 TAB 4, click OK with left mouse

    In CASD and FLOWVIS, Mouse can be used for most commands

    Mouse buttons are shown as: , ,

    If alternate ways of typing is indicated, they are separated by an OR

    This exercise is to prepare and simulate a gas explosion in the 8m wide Advantica fullscale rig (HIGH-A conf.)

    - An existing geometry model will be opened in the preprocessor CASD

    - A simulation mesh will be prepared

    - Porosity calculation will be run (mapping of geometry information onto the grid)

    - The explosion scenario and result output will be defined

    - The FLACS simulation will be run

    - The simulation results will be studied in postprocessor FLOWVIS- If time allows, different ignition locations will be applied

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    Exercise Ib: Explosion simulation in offshore moduleTO BE TYPED: Explanation:

    Initialising and starting the preprocessor CASD

    mkdir YOUR_NAME UNIX: make a distinct catalog in which you perform the exercise

    cd YOUR_NAME UNIX: move into this directory

    cp ~/GEO/*00001* . UNIX: copy setup files and geometry files for the exercise

    f81 UNIX: script to initialize for FLACS-v8.1

    run casd UNIX: command starting up the preprocessor CASD

    Open and view the geometry in CASD (Move cursor to the CASD window)

    choose OPEN in the FILE menu ORfile open OR ALT-f o CASD Ask for opening an existing job file

    choose 100001.caj CASD: Open jobfile 100001, using mouse button

    if any error message appears click CASD: Ignore error message => error message

    Make a grid (mesh) for the simulation, calculate porosities (module dim.: 25.6m x 8m x 8m, origin in corner below the control room)

    Choose SIMULATION_VOLUME from GRID menu OR ALT-r v CASD: To enter the extension of the simulation domain

    Enter -16 -8 0 40 16 16 CASD: Volume is defined (16m out from vent, 8m to the sides)

    In GRID menu, choose DIRECTION X, REGION and enter 56 CASD: 56 grid cells chosen (1.0m grid size).

    Use mouse OR grid dir y reg24 dir z reg 16 CASD: 24 cells in Y-direction and 16 cells in Z-direction

    Type grid info for quality assurance, and to close window CASD: Check that grid dimension is 1.0m as intended

    Choose SAVE from the FILE menu OR ALT-f s CASD: Save geometry and grid files

    Choose CALCULATE from POROSITIES menu OR ALT-p c CASD: Map geometry information onto the grid, porcalc

    Click in the window that pops up PORCALC: Start calculations

    Choose DISPLAY OFF in the GRID menus CASD: Dont draw the grid anymore

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    Exercise Ic: Explosion simulation in offshore moduleTO BE TYPED: Explanation:

    Define explosion scenario

    Choose MONITOR_POINTS in SCENARIO menu

    OR scen mon CASD: Define where to measure variables

    click, and 0.8 4.7 7.9 CASD: Add and define location of monitor point 1

    repeat this for point 2 (12.3, 4, 0.1) and point 3 (24, 7.9, 7.9) CASD: To edit a non-highlighted monitor, click on its number

    Click CASD: Close MONITOR_POINT window

    Choose SINGLE_FIELD_SCALAR from SCENARIO menu CASD: Define which variables to report at monitors

    Click on

    , drag mouse pushing across all monitors, CASD: Log pressure at all three transducers

    Repeat for and CASD: Log pressure impulse and dynamic pressure, too

    Click and choose SINGLE_FIELD_3D from SCENARIO menu CASD: Define variables for contour plots

    Click on

    , CTRL-, CTRL-, CASD: Pressure, flame and velocity vectors. CTRL needed to

    select more than one (NB! deselect when using the scroll bar)

    Choose SIMULATION in SCENARIO menu OR scen sim CASD: Choose output and simulation parameters

    Click on , enter 50 , CASD: Increase number of contour plots, return to main menu

    Click on GAS_COMP... in SCENARIO menu OR scen gas_c CASD: Define gas cloud loc., size, comp. and concentration

    Click on , 0 0 0 CASD: Position of bounding box describing gas cloud

    Click on , 25.6 8 8 CASD: Dimension of gas cloud equals module dimensions

    Click on , 91.7 7

    1.3 CASD: Gas composition is defined

    Click on 1.05 0 CASD: Slightly rich gas mixture is chosen ER=1.05

    Click on IGNITION in SCENARIO menu

    12.5 4.1 4.25

    OR scen ign pos 12.5 4.1 4.25 OK CASD: Define location of ignition (12.5, 4.1, 4.25)

    Choose SAVE from the FILE menu OR ALT-f s CASD: Save all files, ready to run flacs

    Iconise CASD, click at POINT in right corner of CASD frame CASD: Leave CASD for now, can be activated easily

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    Exercise Id: Explosion simulation in offshore moduleTO BE TYPED: Explanation:

    Start FLACS simulation, start preprocessor Flowvis(Move cursor to unix-shell)

    run flacs 100001 UNIX: Start FLACS simulation

    more tt100001 UNIX: Study log-file, give next page, new line

    run flowvis UNIX: Start postprocessor FLOWVIS

    tail -f tt100001 UNIX: Study tail of log file continuously (end with CTRL-C)

    STUDY RESULTS IN POSTPROCESSOR FLOWVIS:

    choose ADD from LAYOUT menu, click centrally in window FLOWVIS: Prepare first layoutclick , choose PLOT_TYPE and SCALAR_TIME plot FLOWVIS: Plotting of time histories of variables

    choose 100001 and P with , select all 3 monitors (drag mouse) FLOWVIS: Plot pressure time history at all monitors

    FLOWVIS: if sim. is running rescan will update plot

    Choose MODIFY in the LAYOUT menu, enter 1 2 FLOWVIS: divide plot into 2 layouts

    Click at lower frame, then , PLOT_TYPE, SCALAR_TIME_ANNO FLOWVIS: show numerical values from pressure plots

    ADD layout and do the same for the DRAG and PIMP variables

    Choose ADD in LAYOUT menu, click, PLOT_TYPE, 2D... FLOWVIS: prepare 2D contour plot

    Choose 100001, P, click FLOWVIS: contour plot of pressure

    click, choose PLOT_SPECIFICATION

    deselect GRID/AXIS, select GEOMETRY FLOWVIS: make plot more readable

    click, choose PLOT_DOMAIN, change k-index to 5 FLOWVIS: choose XY-cut plane through ignition

    Time steps can now be changed moving the lower scroll bar to the right, layout can be varied using the upper scroll bar

    Try to show PRESSURE, repeat this method for PROD and VVEC variables FLOWVIS: visualize flame and velocity vectors

    Try to show PRESSURE and PROD on the same page using LAYOUT MODIFY

    Now that you are familiar with FLOWVIS, try the volume plot menu (select only a job-number not a variable) to study the geometry

    Use PLOT SPECIFICATION to switch on geometry drawing and PLOT DOMAIN to narrow the view window and see below the ceiling

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    Exercise Ie: Explosion simulation in offshore module

    If time allows, study the effect of ignition location:Enter CASD, open the 100001.caj job-file, save this as a new job number e.g. 100002.caj

    Change ignition location in order to study how pressures may vary with different ignition locations

    A) End ignition (0.5, 4.1, 4.25), (job number 100002)

    B) Your own assumed worst-case location (job number 100003)

    Report highest pressure achieved on monitor point

    Make mpg-animation of either 2D or volume plots using the export menu (with all timesteps)

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    A) Enter CASD and build geometry

    Start CASD: run casd

    Use Save as option to save job as 200000.caj [accept possible error messages about co-file etc.]

    Choose EDIT FILE option in the GEOMETRY menu geometry will be built in the new window

    ADD BOX [pos 10, -10, -1, size 40, 25, 1, hue 140, keep all porosities=0] ground is added

    Choose MAXIMIZE from VIEW menu to see the full geometry

    ADD BOX [pos 0, 0, 0, size 0.01, 4.5, 4.5, hue 210] rear wall of boxADD COPY, EDIT PROPERTIES [change first position from 0 to 9] define front wall of box

    ADD COPY, EDIT PROP.. [pos 8, 0.66, 0.66 size 2, 3.18, 3.18], ADD LEFT_DIFF make vent opening in front wall

    ADD BOX [pos 0,0,0 size 9, 0.01, 4.5, hue 210], ADD COPY, EDIT PROP [pos 0,4.5,0] side walls

    ADD BOX [pos 0,0,4.5 size 9,4.5, 0.01, hue 210] roof is added

    Choose ADD UNION 5 times connect primitives in the geometry string

    ADD CYLINDER [pos 1, 0, 0.225 dia 0.18, len 4.5, dir Y, hue 0] make cylinder obstruction

    EDIT DUPLICATE [no 4, delta 0, 0, 0.9] make 4 more cylinders at same X-location

    EDIT DUPLICATE [no 3, delta 2, 0, 0] make 3 more rows of cylinders at this Z-posEDIT DUPLICATE [no 1, delta 1, 0, 0.45] make 4 more rows, with shift in Z-pos

    ADD UNION connect to rest of geometry

    ADD BOX [pos 22, 1, 0, size 2.5, 2.5, 2.5, hue 0] create one target outside box

    ADD UNION connect object primitives

    Geometry is now complete, choose FILE SAVE, FILE EXIT [answer yes when asked]

    Use view options [3D_VIEW and thereafter SHADE in VIEW menu]

    Exercise II: Geometry building & pressure wave propagation

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    Exercise IIIb: Blast propagationGrid will now be defined

    B) Make grid, save and calculate porosities

    Choose GRID SIMULATION_VOLUME [min 0, -9, 0 max 30, 13.5, 13.5] choose grid extent

    GRID DIR X, GRID REGION 60, GRID DIR Y, REGION 45, DIR Z REG 27 define regular 0.50m grid

    Press CTRL-G 9 times, choose GRID STRETCH POS OK OK stretch grid upwards

    GRID DIR Y, CTRL-o, repeat CTRL-SHIFT-G until 9 to 1 (m) is selected select Y-grid lines for y < -1

    GRID STRETCH NEG OK OK stretch negative Y

    GRID DIR X, GRID DIR Y, repeat CTRL-G until 5.5 to 13.5 (m) is selected select Y-grid lines for y > 5.5mGRID STRETCH POS OK OK stretch positive Y

    GRID INFORMATION [close window by OK] check that grid is OK

    (if something goes wrong, start again with choosing simulation volume, direction and region for the direction where things went wrong)

    FILE SAVE, OK, POROSITIES CALCULATE, CALCULATE save grid, calculate porosities

    Geometry is now complete, choose FILE SAVE, FILE EXIT [answer yes when asked] to leave child window and return to main window

    Use view options [open inventor symbols to the right + mouse left and central button to study the geometry.]

    Box 9m x 4.5m x 4.5m box

    with 40 cylinders D= 0.18m

    Vent opening is 3.18m x 3.18m

    (50% of 4.5m x 4.5m end wall)

    Picture shows 3 boxes, only nearest

    one is used in this exercise

    Picture from similar tests at

    Advantica tests site Spadeadam UK

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    Exercise IIc: Blast propagationC) Define scenario for calculations

    SCENARIO MONITOR_POINTS, choose ADD, EDIT [pos 1, 2.25, 1.25] Define first monitor pointChoose COPY and thereafter ADD 5 times Define points along the axis

    use EDIT to change first position to 6, 15, 21.5, 23 and 25 for points 2-6 Modify X-coordinate

    Select point at 23m, change 3rd position to 2.75m, exit monitor points menu Put points at top of target box

    SCENARIO SINGLE_FIELD_SCALAR choose P, select all 6 monitors with left-mouse Select pressure to be recorded

    Repeat for variables PIMP, PROD, UVW Pressure impulse, flame and velocity

    SCENARIO_SINGLE_FIELD_3D_ choose P, PROD, VVEC (+U, V, W) and PMAX Remember CTRL-button selecting multiple

    SCENARIO SIMULATION_AND choose NPLOT=25, then DTPLOT=0.025 Output options

    SCENARIO BOUNDARY choose XLO edit, type PLANE_WAVE, copy/paste to all Non-reflecting boundary cond. everywhereSCEN GAS_COMP, DIM [9, 4.5, 4.5], VOL FRAC [meth 91, ethane 7, propane 2], EQUI [1.05, 0]Define natural gas in box

    SCENARIO IGNITION, POS [0.1, 2.25, 2.25] Ignition at rear wall

    FILE SAVE 200000.caj and exit CASD

    Start simulation in LINUX window: run flacs 200000, check how tt200000 starts up (more tt200000)

    D) Result viewing in flowvis

    How to operate flowvis you should know from previous exercise, limited explanation is therefore given here.

    Study pressure curves at different locations (if in doubt where the monitor points are, use a MONITOR plot option)

    Study the 2D-field variables, P, PMAX, PROD, VVEC

    If time allows, make a VOLUME plot and animation of this [see hints in the flowvis presentation]

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    Exercise IId: Blast propagation

    Comparison: experiments by Shell Global Solutions /Advantica (Phase 3B)

    40 pipes and 10.1m2 vent (50%) [exact pipe and sensor locations may deviate]

    Pressure inside box Pressure at target 13m

    Multi-energy method estimate (strong curve 7 or higher) 17.5m away from cloud centre

    4893491971197713 m outside free-field blast (mbarg)

    100%50%20%10%3%Yield factor4893491971197713 m outside free-

    field blast (mbarg)

    100%50%20%10%3%Yield factor

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    Exercise III: Explosion mitigationApply the test geometry from Exercise I, and investigate how pressures can be reduced

    A) Deluge:Open job-files from Exercise I, add a water deluge system and save as new job-number (100004.caj etc.)

    Possible systems are:

    The FACTORS are calculated based on the water application rate (WAR), which were 16 litre/minute/sqm (MV57) and 26 litre/minute/sqm,(LDN). The simplified relations F1 = 0.23 x WAR and F2 = 4.5 / WAR are used. Simulate two ignition points and one deluge system withFLACS, compare pressure curves of new calculations with dry tests, and also with Interim Guidance Note from Steel Construction Institute.

    DELUGE SYSTEM POSITION SIZE VOLUME_FRACTION MEAN_DROPLET_DIA... NOZZLE_TYPE

    MV57 (TYPE I) -1, 0, 0 27.6 8.0 8.0 0.2 846 FACTORS:3.73,0.284

    LDN (TYPE II) -1, 0, 0 27.6 8.0 8.0 0.2 1280 FACTORS:5.98,0.173

    B) Pressure relief panels (remove water deluge before saving as new job number 100006.caj):

    Define the following panel on North wall (Y=8), evaluate how the relief panels will influence pressures for worst-case ignition location.

    POSITION SIZE MATERIAL PANEL_TYPE OPE.._PR..._DIFF... IN.._AND_FI.._POR.. WEIGHT PANEL_SUBS...

    4, 8, 0 12, 0, 8 DefaultMaterial HINGED 0.05, 0.05 0, 0.8 7 0.7, 1

    C) Inert gas (remove panels and deluge before saving as 100007.caj):

    Add CO2 to the gas mixture, so that the amounts of CO2 is similar to the amount of flammable gas (same volume fraction gives

    about 8-9% in final mixture). How will this influence pressures of the explosion, choose one ignition point?

    D) Geometry change (remove inert gas, deluge and panel before saving as 100008.caj):

    The room between the two control rooms in the test geometry may influence the pressure. Close this room by adding a 16m x 4m x 4m

    BOX at POSITION (4, 0, 4). Simulate one scenario to consider the effect of closing the gap and compare to base case.

    HINT, use GEOMETRY EDIT FILE, ADD (and define) BOX and ADD UNION