Top Banner
GSFC· 2015 A Comparison of Geometric Discretization Methods Douglas P. Bell CRTech
18

A Comparison of Geometric Discretization Methods · • Parabolic trough –Source surface emitting parallel rays –Black-body collector tube at trough focus –1 million rays from

Jan 30, 2021

Download

Documents

dariahiddleston
Welcome message from author
This document is posted to help you gain knowledge. Please leave a comment to let me know what you think about it! Share it to your friends and learn new things together.
Transcript
  • GSFC· 2015

    A Comparison of

    Geometric Discretization

    MethodsDouglas P. Bell

    CRTech

  • Background

    • Thermal analyses often require a system-level model

    – Quick evaluation of the overall system

    – Interactions between components

    – Boundary conditions for component-level models

    • System-level models should

    – Adequately represent components

    • Accurate mass drives transient solution accuracy

    • Accurate area drives convection and radiation accuracy

    – Run quickly for evaluating design space or design changes

    – Correlate to test data

    • This presentation will focus on discretization methods

    appropriate for system-level models

    – Compare models created with various discretization methods

    – Evaluate the strengths and weaknesses of each method

    2TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD

  • Discretization Methods

    • Finite Difference

    – Geometry defined using geometric primitive shapes

    • Flat Finite Elements

    – Structured or unstructured meshes define geometry shape

    – Curved geometry is faceted, requiring many elements

    • Curved Elements

    – Curved geometry is accurately represented using few elements

    – Tessellated and exact options for radiation calculations

    • Tessellated subdivides curved surface elements using facets with

    area correction factors

    • Exact uses precise geometric representation

    3TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD

  • Conduction and Radiation Model

    • Reaction wheel with thermal

    strap

    • Conduction and radiation

    boundary conditions

    • Radiation*

    – Minimum 10k rays per node

    – 1% statistical error

    – Maximum 1M rays per node

    • Transient thermal solution

    4TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD

    * Not typical values; purposefully over-resolved

  • Reaction Wheel Models with ~500 Nodes

    TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD 5

    477 nodes 533 nodes

    533 nodes

    Finite Difference Flat Elements

    Curved Elements

  • 0.00%

    1.00%

    2.00%

    3.00%

    4.00%

    5.00%

    6.00%

    7.00%

    8.00%

    0 500 1000 1500 2000 2500 3000 3500

    Err

    or

    Node Count

    Finite Difference

    Flat Elements

    Curved Element - Tessellated

    Curved Element - Exact

    Reaction Wheel Mass Accuracy

    6TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD

    Flat elements underestimate model mass

  • Reaction Wheel Solution Time vs Node Count

    7TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD

    0

    50

    100

    150

    200

    250

    0 500 1000 1500 2000 2500 3000 3500

    Solu

    tion tim

    e (

    s)

    Node Count

    All methods

    Minimizing node count is important to solution speed

  • Reaction Wheel Radk Calculation Time

    0

    100

    200

    300

    400

    500

    600

    Finite Difference Flat Elements Curved Element - Tessellated

    Ca

    lcu

    latio

    n tim

    e (

    s)

  • Reaction Wheel Solution Time

    9TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD

    0

    20

    40

    60

    80

    100

    120

    140

    160

    180

    Finite Difference Flat Elements Curved Element - Tessellated

    Solu

    tion tim

    e (

    s)

  • Reaction Wheel Discussion

    • Geometry accuracy– Finite difference and curved elements provide accurate mass and

    surface area at all model sizes

    – Flat elements require more nodes for mass and surface area accuracy

    • Calculation time– Flat element model must be increased in size to improve mass

    accuracy• Decreases efficiency of the model

    – Solution times are dependent on node count• Solutions may be repeated many times

    • Smaller models are better

    – The exact method for curved elements is not shown• It is computationally more expensive but only needed for special

    situations (discussed later)

    • Conclusion– Finite difference and curved elements are the better options

    • Curved elements allow arbitrary geometry

    10TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD

  • Geometries Benefitting from Curved Elements

    TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD 11

  • Precision Radiation Model

    12TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD

    • Parabolic trough

    – Source surface emitting parallel rays

    – Black-body collector tube at trough focus

    – 1 million rays from source

    • Reflection must be precise

    – All radiation should be absorbed by collector

    • Bijspace represents poor reflection of rays

    • Special case that requires precise reflections

  • Parabolic Trough with 10 Nodes

    TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD 13

    Curved Element -

    Tessellated

    Curved Elements -

    Exact

    Flat ElementsFinite Difference

  • Precision Radiation Model Discussion

    • Curved elements with exact radiation and finite difference are intrinsically accurate regardless of model size

    • Flat elements and tessellated curved elements can get the correct answer, however…– Flat elements require more nodes

    – Tessellated curved elements require more nodes and/or tessellations

    – Trial and error required to find the model that gives the “correct” answer

    • Multiple runs for trial and error increase the cost

    • Not all models have a predetermined answer: what is “correct”?

    – Increased node count will increase solution time

    • Not all geometries can be represented by finite difference objects

    14TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD

  • Compound Paraboloid

    • Otherwise known as Winston cone

    – Radiator enhancer and shade

    – Solar concentrator

    • Accurate representation requires

    curved elements or many flat

    elements

    15TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD

  • Odd-shaped Mirrors

    16TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD

  • Discretization Method Comparison

    Method Strengths Weaknesses

    Finite Difference • Extremely low node count

    possible

    • Accurate geometry

    • Precise radiation with few

    nodes

    • Fast radiation calculations

    • Limited shapes

    Finite Element • Arbitrary shapes • Requires many nodes to

    represent curvature

    Curved Element

    • Tessellated

    radiation

    • Arbitrary shapes

    • Accurate geometry

    • Fast radiation calculations

    • Requires many nodes count

    or tessellations for precise

    reflections from curved

    surfaces

    Curved Element

    • Exact radiation

    • Arbitrary shapes

    • Accurate geometry

    • Precise radiation calculations

    with few nodes

    • Slower radiation calculations

    17TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD

  • Conclusions

    • Use finite difference objects– For system-level models when geometry can be represented

    with provided geometric primitives

    – Early in design process when CAD geometry or access to a direct modeler (such as SpaceClaim) is not available

    • Use curved elements– For system-level models with arbitrary geometry

    – Early in the design process along with a direct modeler for concept designs

    – With tessellation option when precise radiation is not required

    – With exact option for optics or concentrators

    • Use flat finite elements– For arbitrary geometry

    • Without curvature

    • When high node count is required for temperature gradients

    18TFAWS 2015 – August 3-7, 2015 – Silver Spring, MD