Attachment - 17 EHRM Bonham -Simulation Main Computer Rm 1- CFD Analysis.pdf

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Z2DA--EHRM Bonham, TX Construction 549A4-21-700 EHRM Construction (VA-23-00092679)
Solicitation number
36C77624B0007
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About this file

This CFD analysis report details simulations conducted for the Main Computer Room of the VA medical center in Bonham, TX. The analysis modeled one 70kW CRAC unit operating at full capacity to cool fully-loaded data center equipment in an initial room temperature of 85 degrees Fahrenheit. Over a 10-minute transient simulation, the average room temperature dropped to 74 degrees Fahrenheit with inlet temperatures to racks ranging from 64 to 77 degrees Fahrenheit and outlet temperatures of 82 to 86 degrees Fahrenheit. The simulation determined that a single unit at full output could sufficiently cool the space and equipment. Key metrics analyzed included temperature distributions, airflow vectors, component temperatures, and fluid forces on walls. Accompanying visuals depict results from various viewpoints and planes.

The related federal contract opportunity is for construction services for EHRM projects at the VA medical center in Bonham, TX, solicited by the VA Technology Acquisition Center in Austin under solicitation number 36C77624B0007. The opportunity involves construction of a new MCR and aims to incorporate the thermal analysis findings to adequately cool IT infrastructure as the facility is built out.

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Text version

EHRM BONHAM - MCR –

ONE UNIT FULL CAPACITY

CFD ANALYSIS

Prepared by: Spur Design, BAJ

Date: Monday, June 19, 2023

Spur Design

EHRM Bonham - MCR - CFD Analysis.cfdst Prepared by: Blake Juett

Page 1 Generated with Autodesk CFD 2021

Report Contents

Summary _________________________________________________________________________________________________ 2

Description ________________________________________________________________________________________________________2

Design 1___________________________________________________________________________________________________ 3

One Unit Full Capacity ____________________________________________________________________________________________3

Materials ________________________________________________________________________________________________________3

Boundary Conditions __________________________________________________________________________________________5

Initial Conditions _______________________________________________________________________________________________5

Mesh _____________________________________________________________________________________________________________6

Physics __________________________________________________________________________________________________________7

Solver Settings __________________________________________________________________________________________________7

Convergence ____________________________________________________________________________________________________7

Results __________________________________________________________________________________________________________8

Decision Center _________________________________________________________________________________________ 11

Summary Images ________________________________________________________________________________________________ 11

XY Plane Temperature Billboard – View 1 __________________________________________________________________ 11

XY Plane Temperature Billboard – View 2 __________________________________________________________________ 12

YZ Plane Temperature Billboard – View 1 __________________________________________________________________ 13

YZ Plane Temperature Billboard – View 2 __________________________________________________________________ 14

Airflow Streamer – View 1 ___________________________________________________________________________________ 15

Airflow Streamer – View 2 ___________________________________________________________________________________ 16

Page 2 Generated with Autodesk CFD 2021

Summary

DESCRIPTION

This report contains the results and images from a CFD simulation of the Main Computer Room

(MCR) for the VA medical center in Bonham, TX. This report displays the findings from a simulation of a MCR using of one 70kW CRAC unit at full capacity to cool data center equipment running at full load. The initial temperature of the room was set to 85 degrees Fahrenheit. This was a transient analysis that ran for roughly 10 minutes. At the end of the 10 minutes the average room temperature was 74 degrees Fahrenheit. Inlet temperatures into the racks ranged from 64 degrees Fahrenheit to 77 degrees Fahrenheit. Outlet temperatures out of the racks ranged from

82 to 86 degrees Fahrenheit. The simulation found that one unit running at full capacity was sufficient in cooling the space and the equipment.

Page 3 Generated with Autodesk CFD 2021

Design 1

Length units foot

Coordinate system Cartesian 3D

ONE UNIT FULL CAPACITY

MATERIALS

Page 4 Generated with Autodesk CFD 2021

NAME ASSIGNED TO PROPERTIES

Air Volume

Density Equation of State

Viscosity 1.817e-05 Pa-s

Conductivity 0.02563 W/m-K

Specific heat 1004.0 J/kg-K

Compressibility 1.4

Emissivity 1.0

Wall roughness 0.0 meter

Phase Vapor Pressure

Stainless Steel

(304)

Part1.1-CRU-514-2

Part1.1-CRU-514-1

Part1.Coils - 1

X-Direction Piecewise Linear

Y-Direction Same as X-dir.

Z-Direction Same as X-dir.

Density 8.0 g/cm3

Specific heat 0.5 J/g-K

Emissivity 0.54

Transmissivity 0.0

Electrical resistivity 7.2e-05 ohm-cm

Glass Wool Part1.1-517-001

Part1.1-517-002

X-Direction 0.038 W/m-K

Z-Direction Same as X-dir.

Density 24.0 kg/m3

Specific heat 700.0 J/kg-K

Emissivity 0.8

Transmissivity 0.0

Electrical resistivity 40000000000000.0

Aluminum

Alloy (6063)

Part1.MDA-B

Part1.MDA-A

Part1.SC - 9

Part1.SC - 7

Part1.SC - 5

Part1.SC - 3

Part1.HDA-A

Part1.SC - 1

Part1.SC - 2

Part1.SC - 4

Part1.SC - 6

Part1.SC - 8

Part1.HDA-B

Part1.MDA-A (1)

Part1.MDA-B (1)

X-Direction 218.0 W/m-K

Z-Direction Same as X-dir.

Density 2.7 g/cm3

Specific heat 0.9 J/g-K

Emissivity 0.2

Transmissivity 0.0

Electrical resistivity 2.99e-06 ohm-cm

Page 5 Generated with Autodesk CFD 2021

Stainless Steel

(304)

Part1.1-CRU-514-2

Part1.1-CRU-514-1

Part1.Coils - 1

X-Direction Piecewise Linear

Z-Direction Same as X-dir.

Density 8.0 g/cm3

Specific heat 0.5 J/g-K

Emissivity 0.54

Transmissivity 0.0

Electrical resistivity 7.2e-05 ohm-cm

DS070 - Full

Cap

Part1.Coils - 2

Flow 9000.0 ft3/min

Heat Transfer Heat Input/Extraction

BOUNDARY CONDITIONS

TYPE ASSIGNED TO

Total Heat Generation(3500 W) Part1.MDA-B

Part1.MDA-A

Part1.SC - 9

Part1.SC - 7

Part1.SC - 5

Part1.SC - 3

Part1.SC - 1

Part1.SC - 2

Part1.SC - 4

Part1.SC - 6

Part1.SC - 8

Part1.MDA-A (1)

Part1.MDA-B (1)

Total Heat Generation(2800 W) Part1.HDA-A

Part1.HDA-B

Film Coefficient(3.5

BTU/ft2/h/F, 100 Fahrenheit)

Surface:128

Surface:129

Surface:130

Surface:133

Surface:134

Surface:171

INITIAL CONDITIONS

TYPE ASSIGNED TO

Temperature(85 Fahrenheit) Volume

Page 6 Generated with Autodesk CFD 2021

MESH

Automatic Meshing Settings

Surface refinement 0

Gap refinement 0

Resolution factor 1.0

Edge growth rate 1.1

Minimum points on edge 2

Points on longest edge 10

Surface limiting aspect ratio 20

Mesh Enhancement Settings

Mesh enhancement 1

Enhancement blending 0

Number of layers 3

Layer factor 0.45

Layer gradation 1.05

Meshed Model

Number of Nodes 44924

Number of Elements 169068

Page 7 Generated with Autodesk CFD 2021

PHYSICS

Flow On

Compressibility Incompressible

Heat Transfer On

Auto Forced Convection Off

Gravity Components 0.0, 0.0, -32.174

Radiation On

Scalar No scalar

Turbulence On

SOLVER SETTINGS

Solution mode Transient

Solver computer MyComputer

Intelligent solution control Off

Advection scheme ADV 5

Turbulence model k-epsilon

CONVERGENCE

Iterations run 600

Solve time 703 seconds

Solver version 21.0.20201120

Energy Balance

Fluid Energy Balance Information (numerical) energy out - 2.4542 Btu/s heat transfer due to sources in 0.0 Btu/s heat transfer from wall to fluid 39.557 Btu/s mdotin x cp x (tout - tin) -64.858 Btu/s radiation heat balance 0.0 4.0969

Solid Energy Balance Information heat transfer due to sources in 48.39 Btu/s heat transfer from exterior to 0.50716 Btu/s heat transfer from fluid to solid -39.557 Btu/s

Mass Balance

IN OUT

Mass flow 0.0 0.0

Volume flow 0.0 f^3/s 0.0 f^3/s

Page 8 Generated with Autodesk CFD 2021

RESULTS

Inlets and Outlets inlet 1 (heat exchanger outlet - part 2) inlet bulk pressure 7.09059 psf inlet bulk temperature 52.342 F inlet mach number 0.00932077 mass flow in 0.360849 minimum x,y,z of 0.0 node near minimum 5.0 reynolds number 258657.0 surface id 23.0 volume flow in 150.0 f^3/s inlet 2 (heat exchanger inlet - part 2) inlet bulk pressure 6.49373 psf inlet bulk temperature 76.1682 F inlet mach number 0.00911119 mass flow in -0.344805 minimum x,y,z of 0.0

Page 9 Generated with Autodesk CFD 2021 node near minimum 18.0 reynolds number 247157.0 surface id 24.0 total mass flow in 0.0160442 total vol. flow in 0.00334594 f^3/s volume flow in -149.997 f^3/s inlet 1 (heat exchanger outlet - part 2) inlet bulk pressure 7.09059 psf inlet bulk temperature 52.342 F inlet mach number 0.00932077 mass flow in 0.360849 minimum x,y,z of 0.0 node near minimum 5.0 reynolds number 258657.0 surface id 23.0 volume flow in 150.0 f^3/s

Field Variable Results

VARIABLE MAX MIN

cond 0.0349583 B/f-s-R 4.11001e-06 B/f-s-R dens 15.5086 lbf-s^2/f^4 0.00222363 lbf-s^2/f^4 econd 0.0593352 B/f-s-R 0.0 B/f-s-R emiss 1.0 0.0 evisc 0.020048 lbf-s/f^2 0.0 lbf-s/f^2 gent 602.215 1/s 0.0145279 1/s press 7.19775 psf 0.0 psf ptotl 7.57063 psf 0.0 psf scal1 0.0 0.0 seebeck 0.0 V/K 0.0 V/K shgc 0.0 0.0 spech 7.71567 B-f/lbf-s^2R 3.84246 B-f/lbf-s^2R temp 100.909 F 55.342 F transmiss 0.0 0.0 turbd 753.229 f^2/s^3 1.49389e-07 f^2/s^3 turbk 106.502 f^2/s^2 3.79148e-10 f^2/s^2 ufactor 0.0 0.0 visc 3.79148e-07 lbf-s/f^2 0.0 lbf-s/f^2 vx vel 8.69385 f/s -37.1593 f/s vy vel 35.7109 f/s -11.6361 f/s vz vel 10.8389 f/s -37.7388 f/s wrough 0.0 f 0.0 f

Page 10 Generated with Autodesk CFD 2021

Component Thermal Summary

PART MINIMUM

TEMPERATURE

MAXIMUM

TEMPERATURE

VOLUME AVERAGED

TEMPERATURE

Part1.1-CRU-514-2 55.342 80.2455 72.375

Part1.Coils - 2 0 0 0

Part1.MDA-B 68.266 82.7425 76.8078

Part1.MDA-A 70.9232 82.5556 76.8648

Part1.SC - 9 74.4534 85.4609 78.6439

Part1.SC - 7 73.3556 86.5423 80.0479

Part1.SC - 5 74.3476 86.5073 80.3858

Part1.SC - 3 76.0896 86.4799 80.6594

Part1.HDA-A 75.3606 83.0263 76.9208

Part1.1-517-001 55.342 100.126 86.8117

Part1.1-517-002 66.174 100.909 90.4619

Part1.SC - 1 72.3593 86.4691 80.0547

Part1.SC - 2 76.4927 86.4003 80.7167

Part1.SC - 4 77.0326 86.3984 80.5235

Part1.SC - 6 74.8967 86.5321 80.2708

Part1.SC - 8 73.5307 86.5543 79.8667

Part1.HDA-B 64.2455 83.0721 75.0263

Part1.MDA-A (1) 67.6527 82.6822 76.8685

Part1.MDA-B (1) 65.8973 82.538 76.5788

Part1.1-CRU-514-1 73.5457 80.5604 75.2292

Part1.Coils - 1 74.531 81.8478 75.3625

Volume 55.342 86.3419 73.679

Fluid Forces on Walls pressx 0.9841 pounds pressy -0.52438 pounds pressz -0.21 pounds shearx -0.01630 pounds sheary -0.010503 pounds shearz -0.034964 pounds

Page 11 Generated with Autodesk CFD 2021

Decision Center

SUMMARY IMAGES

XY PLANE TEMPERATURE BILLBOARD – VIEW 1

Temperature Distribution with Directional Airflow Vectors.

Page 12 Generated with Autodesk CFD 2021

XY PLANE TEMPERATURE BILLBOARD – VIEW 2

Page 13 Generated with Autodesk CFD 2021

YZ PLANE TEMPERATURE BILLBOARD – VIEW 1

Page 14 Generated with Autodesk CFD 2021

YZ PLANE TEMPERATURE BILLBOARD – VIEW 2

Page 15 Generated with Autodesk CFD 2021

AIRFLOW STREAMER – VIEW 1

Directional Airflow Streamers Colored by Temperature.

Page 16 Generated with Autodesk CFD 2021

AIRFLOW STREAMER – VIEW 2

Directional Airflow Streamers Colored by Temperature.

File details come from the government source that posted it. Updated .