me final presentation

Upload: mechstar-santhosh

Post on 06-Apr-2018

222 views

Category:

Documents


0 download

TRANSCRIPT

  • 8/2/2019 Me Final Presentation

    1/22

    Thermal and Structural Analysis of a

    Combustion Test Apparatus using

    ANSYSAdam Decker

    Brandon Underwood

    Matt Greathouse

    Scott Andrews

    ME 450 Dr. Nemah MW 430 PM 545 PM

    Fall 2008

  • 8/2/2019 Me Final Presentation

    2/22

    Objectives

    Structural Analysis on the fuel tank filled with

    a propane and air mixture if an explosion

    occurs.

    Transient Thermal Analysis on the test cell to

    test if the temperatures will be too high for

    the current design.

  • 8/2/2019 Me Final Presentation

    3/22

    Introduction

    Tank

    Test Cell

  • 8/2/2019 Me Final Presentation

    4/22

    Theoretical Background

  • 8/2/2019 Me Final Presentation

    5/22

    Combustion

    Chamber Heat

    Transfer Analysis

    A simulation wasrun to find

    whether the entire

    chamber could

    heat to the point

    where any special

    precautions would

    need to be taken.

  • 8/2/2019 Me Final Presentation

    6/22

    Fuel/Air Mix Behavior

    What would the characteristics be of the fuel/air

    mixture during the combustion process?

    What equations would be needed to find this

    information?

    What is the convection heat transfer coefficient,

    enabling ANSYS to simulate the heat transfer

    from the combustion to the chamber walls?

  • 8/2/2019 Me Final Presentation

    7/22

    Equations

    1. Hydraulic Diameter

    2. Reynolds Number

    3. Friction Factor

    4. Nusselt Number

    5. Convection Coefficient

  • 8/2/2019 Me Final Presentation

    8/22

    Tank Explosion

    Analysis

    A simulation wasrun to predict what

    could happen if

    multiple part

    failures were to

    occur causing the

    ignition of the

    tanks fuel/air mix.

  • 8/2/2019 Me Final Presentation

    9/22

    Maximum Pressure

    First, find the maximum possible pressure for

    the combustion temperature using ideal gas

    law.

    PV=nRTDouble this pressure to simulate the combustion

    shockwave.

  • 8/2/2019 Me Final Presentation

    10/22

    Explosion analysis model details

    Modeled in ProE

    Imported into ANSYS

    Workbench

    Static structural analysis 7285 nodes

    3605 elements

  • 8/2/2019 Me Final Presentation

    11/22

    Materials and conditions

    Structural steel

    0 DOF on base of tank

    Constant 20 C temperature 36259 psi Yield strength

    66717 psi Ultimate strength

  • 8/2/2019 Me Final Presentation

    12/22

    Application of loads

    Steps Time [s] Pressure [psi]

    10. 0.

    1.e-002 3000.

    22.e-002

    1442.79.

    3 10. 0.

    Pressure loading on

    interior surface

    10ms overpressure

    simulates shock wave ofexplosion

    Ramp loading better

    simulates real world

    behavior

  • 8/2/2019 Me Final Presentation

    13/22

    Tank analysis results

    42897 psi maximum

    stress

    Greater than yield

    stress Less than ultimate

    stress of 66717 psi

    Tank should be replacedif an explosion occurs

  • 8/2/2019 Me Final Presentation

    14/22

    Thermal analysis model details

    Modeled in ProE

    Imported into ANSYS

    Workbench

    Transient thermalanalysis

    Block contained

    14228 nodes 8112 elements

  • 8/2/2019 Me Final Presentation

    15/22

    Materials and conditions

    Aluminum

    Initially 20 C

    1.5ms for 60%

    combustion

    StepStepEndTime

    InitialTimeStep

    Minimum Time

    Step

    Maximum Time

    Step

    11.5e-003 s

    1.5e-005 s

    1.5e-006 s

    1.5e-004 s

    2 1. s9.985e-

    003 s

    9.985e-

    004 s

    9.985e-

    002 s

    3 2. s1.e-002

    s1.e-003

    s0.1 s

  • 8/2/2019 Me Final Presentation

    16/22

    Application of loads

    Natural convection

    Vertical surfaces

    Horizontal surfaces

    Forced turbulentconvection

    h=5.2527e-005

    BTU/sinF

    Radiation

    =.1

    Steps Time [s]ConvectionCoefficient

    [BTU/sinF]

    Temperature[F]

    1

    0. = 5.2527e-005 = 2240.

    1.5e-0035.2527e-005

    2240.

    2 1. 1340.3

    3 2. 0. 68.

    Steps Time [s] Temperature [F]1

    0. = 2240.

    1.5e-003 2240.

    2 1. 1340.3

    3 2. 32.

  • 8/2/2019 Me Final Presentation

    17/22

    Block analysis results

    Maximum

    temperature 87.231 F

    Temperature on

    outside of blockremains even lower

    No danger to

    components hooked

    up to the outside

  • 8/2/2019 Me Final Presentation

    18/22

    Impact Statement- Societal

    Propane:

    -majority of used is produced domestically

    -nearly 80 percent of farms use to run pumpsand engines, dry crops, heat buildings, process

    foods, and reduce emissions.

    -more than 10 million vehicles around the

    world use propane

  • 8/2/2019 Me Final Presentation

    19/22

    Impact Statement - Environmental

    Propane:

    low carbon count (per BTU)

    emmisions are much cleaner

    has relatively gentle human toxicity characteristics

    not a potential contributor to groundwater

    pollution

  • 8/2/2019 Me Final Presentation

    20/22

    Impact Statement - Safety

    Flammability

    Propane can create gaseous hydrogen (which

    can be a flammable issue)

  • 8/2/2019 Me Final Presentation

    21/22

    Conclusion

    Structural Analysis showed no catastophic

    failures in tank. Will need replaced if a failure

    occurs.

    Thermal analysis showed that the test cell will

    not reach temperatures that could damage

    other components.

  • 8/2/2019 Me Final Presentation

    22/22

    Bibliography

    Moaveni, Saeed. Finite Element Analysis:

    Theory and Application with ANSYS. Upper

    Saddle River: Pearson Prentice Hall, 2008.

    Incropera, Frank P., David P. Dewitt, Theodore

    L. Bergman, and Adrienne S. Lavine.

    Fundamentals of Heat and Mass Transfer.

    Hoboken: John Wiley & Sons Inc., 2007.