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    A Numerical Investigation of Premixed Combustion in Wave Rotors

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 003::page 668
    Author:
    M. R. Nalim
    ,
    D. E. Paxson
    DOI: 10.1115/1.2817036
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Wave rotor cycles that utilize premixed combustion processes within the passages are examined numerically using a one-dimensional CFD-based simulation. Internal-combustion wave rotors are envisioned for use as pressure-gain combustors in gas turbine engines. The simulation methodology is described, including a presentation of the assumed governing equations for the flow and reaction in the channels, the numerical integration method used, and the modeling of external components such as recirculation ducts. A number of cycle simulations are then presented that illustrate both turbulent-deflagration and detonation modes of combustion. Estimates of performance and rotor wall temperatures for the various cycles are made, and the advantages and disadvantages of each are discussed.
    keyword(s): Combustion , Waves , Rotors , Cycles , Explosions , Turbulence , Ducts , Equations , Wall temperature , Combustion chambers , Computational fluid dynamics , Engineering simulation , Gas turbines , Modeling , Channels (Hydraulic engineering) , Pressure AND Flow (Dynamics) ,
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      A Numerical Investigation of Premixed Combustion in Wave Rotors

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/118665
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. R. Nalim
    contributor authorD. E. Paxson
    date accessioned2017-05-08T23:53:25Z
    date available2017-05-08T23:53:25Z
    date copyrightJuly, 1997
    date issued1997
    identifier issn1528-8919
    identifier otherJETPEZ-26766#668_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118665
    description abstractWave rotor cycles that utilize premixed combustion processes within the passages are examined numerically using a one-dimensional CFD-based simulation. Internal-combustion wave rotors are envisioned for use as pressure-gain combustors in gas turbine engines. The simulation methodology is described, including a presentation of the assumed governing equations for the flow and reaction in the channels, the numerical integration method used, and the modeling of external components such as recirculation ducts. A number of cycle simulations are then presented that illustrate both turbulent-deflagration and detonation modes of combustion. Estimates of performance and rotor wall temperatures for the various cycles are made, and the advantages and disadvantages of each are discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Numerical Investigation of Premixed Combustion in Wave Rotors
    typeJournal Paper
    journal volume119
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2817036
    journal fristpage668
    journal lastpage675
    identifier eissn0742-4795
    keywordsCombustion
    keywordsWaves
    keywordsRotors
    keywordsCycles
    keywordsExplosions
    keywordsTurbulence
    keywordsDucts
    keywordsEquations
    keywordsWall temperature
    keywordsCombustion chambers
    keywordsComputational fluid dynamics
    keywordsEngineering simulation
    keywordsGas turbines
    keywordsModeling
    keywordsChannels (Hydraulic engineering)
    keywordsPressure AND Flow (Dynamics)
    treeJournal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 003
    contenttypeFulltext
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