3DYNAPVF™ - Dynaflow, Inc.
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1. The result shown in Figure 2 required the following inputs 1000 Recover File Number 0 15 0 0 0 15 xmin ymin zmin m 0 15 0 0 0 15 xmax ymax zmax m 51 1 51 nx ny nz 0 1 0 0 a b c d 12 DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 Interaction of Two Bubbles Under a Free Surface p 2E 06 1 8E 06 1 6E 06 1 4E 06 1 2E 06 1E 06 800000 600000 400000 200000 108791 73178 0 200000 Figure 3 Flow Field Around Two Bubbles Interacting under a Free Surface The result shown in Figure 4 required the following inputs 1000 Recover file number 0 2 2 xmin ymin zmin m 0 2 1 xmax ymax zmax m 1 81 61 nx ny nz 1 0 0 0 a b c d 13 DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 Flow Field from a Bubble Collapsing Over a Stationary Rigid Cylinder 0 04 0 02 10000 9500 9000 8500 8000 7500 7000 6500 6000 5500 5000 4500 4000 3500 3000 02 0 04 0 06 0 08 0 05 0 0 05 y Figure 4 Flow Field Around a Bubble Collapsing Above a Stationary Rigid Cylinder The result shown in Figure 4 required the following inputs 1200 Recover file number 0 0 07 0 09 xmin ymin zmin m 0 0 07 0 05 xmax ymax zmax m 1 71 1 nx ny 2 1 0 0 0 a b c d 14 DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 Flow Field Around Six Airguns Near Test Panel p 280000 gt 260000 240000 220000 200000 180000 160000 140000 120000 100000 80000 60002. INC 3DYNAPVF USER MANUAL 7 084 n l Ot At These values are then substituted in equation 3 to obtain the pressure The pressure is set to zero if the pressure is negative DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 USING 3DYNAPVF Input Files To start running 3DYNAPVF the user needs to have the following input files DATA_IN REC HHH RECOVER_FSI FIELD_DATA DAT The input files DATA_IN are the same input files used in the 3DYNAFS run The recover file REC Hf is automatically generated after the user runs 3DYNAFS and RECOVER_FSI is automatically generated if running a FSI case In addition the user needs to provide the file FIELD_DATA DAT FIELD_DATA DAT The user needs to specify the size of the computational domain and the number of grid points in FIELD_DATA DAT The user can also specify the plane used to cross cut the domain The plane is defined by ax by cz d An example of the FIELD_DATA DAT is shown below Example Value Variable Name 1000 File umber 0 0 13 xmin ymin zmin 13 13 13 xmax ymax zmax 41 41 81 nxgrid nygrid nzgrid 0 1 0 1 a b c d Line 1 Specify the number of recover file the user wants to compute the flow field Line 2 Specify the coordinates of the lower left point of the computational domain Line 3 Specify the coordinates of the upper right point of the computational domain Line 4 Specify the
3. which is licensed as a single product The software is in use on a computer when it is loaded into the temporary memory i e RAM or installed into the permanent memory e g hard disk or other storage device of that computer You may use the Software on a network provided you have purchased one copy for each user Contact us about multiple user discounts Copyright and Restrictions The software is owned by DYNAFLOW INC and is protected by United States copyright laws You must treat the Software like any other copyrighted material except that you may make one copy of the Software solely for backup archival purposes You may not reverse engineer decompile or disassemble the Software except to the extent applicable law expressly prohibits the foregoing restriction DYNAFLOW INC may have patents and or pending patent applications covering subject matters in this document The furnishing of this document does not give you any license to these patents DYNAFLOW INC grants you a non exclusive license to use one copy of the 3DYNAPVF software for the duration specified in your license agreement document signed by a DYNAFLOW INC official representative Limited Warranty For thirty 30 days from your date of purchase DYNAFLOW INC warrants that the media on which the Software is distributed are free from defects in materials and workmanship DYNAFLOW INC will repair or replace the Software provided that the defective Software me
4. 0 40000 20000 Figure 5 Flow Field Around Six Airguns Near a Test Panel The result shown in Figure 4 required the following inputs 2000 File number 5 2 3 xmin ymin zmin 5 6 3 xmax ymax zmax 4032 1 nxgrid nygrid nzgrid 001 3 acoef bcoef coef d 15
5. ASE STUDIES The following examples illustrate the results obtained with 3DYNAPVF These consist of BUBBLE DYNAMICS IN A GRAVITY FIELD BUBBLE DYNAMICS NEAR AN INFINITE WALL Two BUBBLE INTERACTION UNDER FREE SURFACE BUBBLE DYNAMICS NEAR A STATIONARY RIGID CYLINDER SIX AIRGUNS NEAR A DEFORMABLE BOX FSI CASE In the following pages we present each of these cases to help the user to get used to utilizing 3DYNAPVF 10 DYNAFLOW INC 3DYNAPVE USER MANUAL 7 084 Flow Field Around an Expanding Bubble in Gravity Tips 1 All inputs in this example are in SI units 10 p 1 5E 06 1 4E 06 1 3E 06 1 2E 06 1 1E 06 1E 06 900000 800000 700000 600000 300000 6 4 2 0 2 4 6 Figure 1 Flow Field Around an Expanding Bubble in Gravity The results shown in Figure 1 required the following inputs field_data dat file 800 Recover File Number 6 0 0 2 xmin ymin zmin m 6 0 0 10 xmax ymax zmax m 51 1 51 nx ny nz 0 1 0 0 a b c d 11 DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 Flow Field Around a Bubble near an Infinite Plate Tips 1 Ensure that one of the ends of the zone defined for the flow field is just inside the infinite plate 0 15 0 1 p 1E 06 900000 800000 700000 600000 500000 400000 300000 200000 87808 1 0 05 0 1 0 15 05 Figure 2 Flow Field Around an Expanding Bubble Near an Infinite Plate
6. DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 3DYNAPVE Post Processing Software for 3DYNAFS Pressure and Velocity Field Computation Version 2009 2 April 2009 DYNAFLOW INC 10621 J IRON BRIDGE ROAD Jessup MD 20794 U S A Phone 301 604 3688 Fax 301 604 3689 e mail info dynaflow inc com http www dynaflow inc com DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 TABLE OF CONTENTS TABLE OF 60 0 0 LIST OF FIGURES LICENSE AGREEMENT 0 DESCRIPTION OF 3DYNAPVF USING 3DYNAPVE INPUT FILES ssccccssssscessscccceseee OUTPUT FILES cccccccsssssssssccceees SAMPLE CASE STUDIES DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 LIST OF FIGURES Figure 1 Flow Field Around an Expanding Bubble in 01 11 Figure 2 Flow Field Around an Expanding Bubble Near an Infinite Plate 12 Figure 3 Flow Field Around Two Bubbles Interacting under a Free Surface 13 Figure 4 Flow Field Around a Bubble Collapsing Above a Stationary Rigid CLIN OP varierat hss tecswaa AGATA Oa 14 Figure 5 Flow Field Around Six Airguns Near a Test 170761 15 DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 LICENSE AGREEMENT This agreement governs your use of the 3DYNAPVF product and any material enclosed with it including any manuals disks and computer programs Grant of License This agreement permits you to use one copy of the Software
7. dia is returned to DYNAFLOW INC or an authorized dealer within 30 days from the date of purchase Limitation of Liabilities In no event will DYNAFLOW INC be liable for any indirect special incidental economic or consequential damages arising out of the use of or inability to use the Software In no event will DYNAFLOW INC s liability exceed the amount paid by you for the Software DYNAFLOW makes no expression of suitability of the present product for any purpose except that it will reproduce on a suitable computer the documented cases at the end of this report and work properly for similar cases Restricted Rights No part of this document may be reproduced or transmitted in any form or by any means electronic or mechanical for any purpose without the express written permission of DYNAFLOW INC Other brands or product names are trademarks or registered trademarks of their respective holders DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 DESCRIPTION OF 3DYNAPVF 3DYNAPVE is a post processing program for 3DYNAFS that computes the pressure and velocity fields in a specified space region at a given time step Details of the state of the fluid domain e g the velocity and pressure fields can be obtained by the post processing technique described below 3DYNAPVE is a companion program to the 3DYNAFS code The application of Green s identity equation enables the calculation of the potential at any point ins
8. ide the fluid domain In this case no linear system needs to be solved since at the end of a given time step all the quantities on the boundaries are known In the post processing code the values of potential and normal velocity from the boundaries only i e bubble and boundary surfaces are read from files saved during the execution of the main 3DYNAFST code as are the coordinates and connectivity of the boundary points The discrete equivalent of the Green s identity yields the value of the potential at the desired field point P as og on 00 h ano 2 OG P G Gz 9 Gy H H3 rey Hy e gt 1 90 OnN where Q is the solid angle from which P locally sees the domain Equation 1 enables one to compute the potential on the prescribed grid points These presently form a uniform Cartesian grid of points overlaid on the flow field The grid is entered by the user by choosing the lower left corner and the upper right corner of the grid the number of grid points in the x y and z directions The boundary integral equations are derived from the conservation equations of the fluid and apply to the fluid domain only Thus they are not valid inside solid structures or inside the bubble After the coordinates of the grid points are generated a first pass is made to determine if they are in the fluid or not Points inside bubbles and or bodies are identified and excluded from the following potential computation The ve
9. locity components at these points are presently set to zero For those points inside bubbles DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 the pressure is set equal to the pressure inside the bubble and for those points inside the body the pressure is set to zero The velocity field is given by the potential derivatives For the points in the fluid we use second order central differences to compute the derivatives for example pad 00 2 Ax 2 u x In the case where the point is near the surface of the bubble a simple one sided difference equation is used In addition to the computations of the velocity at the grids the velocities at the bubble nodes are also available These along with all velocities at the grid points are then output to files for graphical processing The pressure at a point in the fluid domain is given by the unsteady Bernoulli equation p o 9 100 06 pore P Po 0 pa zZ 3 where pois the ambient pressure at Zy This requires the knowledge of potential time derivatives The potential time derivatives can also be computed using Green s identity ob 0 Onct Ct 1 og ag 0 Ondt t 2 oF P G Gp EN Gy 2 H des Hy 4 e e 27 2 On t Ot N For a Fluid Structure Interaction FSI case run the potential time derivatives is computed based on a finite difference scheme using potential from two consecutive time steps i e DYNAFLOW
10. number of grid points Line 5 Specify the plane to crosscut the objects Tip The user can specify a two dimensional domain of a 3 D domain by setting the number of grid points of a dimension eg z dimension equal to 1 The user also can DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 compute the flow field at a single point by setting all numbers of grid points equal to 1 ie nxgrid nygrid nzgrid I In this case the coordinates of the considered point are xmin ymin zmin Output Files PV Fett plt This file is for visualization of the result by using Tecplot Tecplot is a visualization program developed by Amtec Engineering Inc This file contains the pressure velocity and potential output generated by the post processing program X Y Z are the coordinates of the grid point U V W are the components of the velocity P and are the pressure and the potential In addition to the Tecplot header at the beginning of the file the file is stored in the following format do 1 nzgrid do j I nygrid do i 1 nxgrid X i j k Z i j k P j k UG Vij W ij k ij k end do end do end do If the user prefers to use another graphing software the file can be edited to remove the Tecplot header and replace by whatever is necessary Dynaflow can also provide a version with another output format if the user so specifies at a norminal fee DYNAFLOW INC 3DYNAPVF USER MANUAL 7 084 SAMPLE C
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