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    Effect of Temperature on Microparticle Rebound Characteristics at Constant Impact Velocity—Part II

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 011::page 112604
    Author:
    Delimont, J. M.
    ,
    Murdock, M. K.
    ,
    Ng, W. F.
    ,
    Ekkad, S. V.
    DOI: 10.1115/1.4030313
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: When gas turbine engines operate in environments where the intake air has some concentration of particles, the engine will experience degradation. Very few studies of such microparticles approaching their melting temperatures are available in open literature. The coefficient of restitution (COR), a measure of the particles' impact characteristics, was measured in this study of microparticles using a particle tracking technique. Part II of this study presents data taken using the Virginia Tech Aerothermal Rig and Arizona road dust (ARD) of 20–40 خ¼m size range. Data were taken at temperatures up to and including 1323 K, where significant deposition of the sand particles was observed. The velocity at which the particles impact the surface was held at a constant 70 m/s for all of the temperature cases. The target on which the particles impacted was made of a nickel alloy, Hastelloy X. The particle angle of impact was also varied between 30 deg and 80 deg. Deposition of particles was observed as some particles approach their glass transition point and became molten. Other particles, which do not become molten due to different particle composition, rebounded and maintained a relatively high COR. Images were taken using a microscope to examine the particle deposition that occurs at various angles. A rebound ratio was formulated to give a measure of the number of particles which deposited on the surface. The results show an increase in deposition as the temperature approaches the melting temperature of sand.
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      Effect of Temperature on Microparticle Rebound Characteristics at Constant Impact Velocity—Part II

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    http://yetl.yabesh.ir/yetl1/handle/yetl/158092
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    contributor authorDelimont, J. M.
    contributor authorMurdock, M. K.
    contributor authorNg, W. F.
    contributor authorEkkad, S. V.
    date accessioned2017-05-09T01:18:24Z
    date available2017-05-09T01:18:24Z
    date issued2015
    identifier issn1528-8919
    identifier othergtp_137_11_112604.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/158092
    description abstractWhen gas turbine engines operate in environments where the intake air has some concentration of particles, the engine will experience degradation. Very few studies of such microparticles approaching their melting temperatures are available in open literature. The coefficient of restitution (COR), a measure of the particles' impact characteristics, was measured in this study of microparticles using a particle tracking technique. Part II of this study presents data taken using the Virginia Tech Aerothermal Rig and Arizona road dust (ARD) of 20–40 خ¼m size range. Data were taken at temperatures up to and including 1323 K, where significant deposition of the sand particles was observed. The velocity at which the particles impact the surface was held at a constant 70 m/s for all of the temperature cases. The target on which the particles impacted was made of a nickel alloy, Hastelloy X. The particle angle of impact was also varied between 30 deg and 80 deg. Deposition of particles was observed as some particles approach their glass transition point and became molten. Other particles, which do not become molten due to different particle composition, rebounded and maintained a relatively high COR. Images were taken using a microscope to examine the particle deposition that occurs at various angles. A rebound ratio was formulated to give a measure of the number of particles which deposited on the surface. The results show an increase in deposition as the temperature approaches the melting temperature of sand.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Temperature on Microparticle Rebound Characteristics at Constant Impact Velocity—Part II
    typeJournal Paper
    journal volume137
    journal issue11
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4030313
    journal fristpage112604
    journal lastpage112604
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 011
    contenttypeFulltext
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