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    Development and Integration of Rain Ingestion Effects in Engine Performance Simulations

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 004::page 41202
    Author:
    Roumeliotis, I.
    ,
    Alexiou, A.
    ,
    Aretakis, N.
    ,
    Sieros, G.
    ,
    Mathioudakis, K.
    DOI: 10.1115/1.4028545
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Rain ingestion can significantly affect the performance and operability of gas turbine aeroengines. In order to study and understand rain ingestion phenomena at engine level, a performance model is required that integrates component models capable of simulating the physics of rain ingestion. The current work provides, for the first time in the open literature, information about the setup of a mixedfidelity engine model suitable for rain ingestion simulation and corresponding overall engine performance results. Such a model can initially support an analysis of rain ingestion during the predesign phase of engine development. Once components and engine models are validated and calibrated versus experimental data, they can then be used to support certification tests, the extrapolation of ground test results to altitude conditions, the evaluation of control or engine hardware improvements and eventually the investigation of inflight events. In the present paper, component models of various levels of fidelity are first described. These models account for the scoop effect at engine inlet, the fan effect and the effects of water presence in the operation and performance of the compressors and the combustor. Phenomena such as velocity slip between the liquid and gaseous phases, droplet breakup, droplet–surface interaction, droplet and film evaporation as well as compressor stages rematching due to evaporation are included in the calculations. Water ingestion influences the operation of the components and their matching, so in order to simulate rain ingestion at engine level, a suitable multifidelity engine model has been developed in the Proosis simulation platform. The engine model's architecture is discussed, and a generic high bypass turbofan is selected as a demonstration test case engine. The analysis of rain ingestion effects on engine performance and operability is performed for the worst case scenario, with respect to the water quantity entering the engine. The results indicate that rain ingestion has a strong negative effect on highpressure compressor surge margin, fuel consumption, and combustor efficiency, while more than half of the water entering the core is expected to remain unevaporated and reach the combustor in the form of film.
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      Development and Integration of Rain Ingestion Effects in Engine Performance Simulations

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    https://yetl.yabesh.ir/yetl1/handle/yetl/157908
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    contributor authorRoumeliotis, I.
    contributor authorAlexiou, A.
    contributor authorAretakis, N.
    contributor authorSieros, G.
    contributor authorMathioudakis, K.
    date accessioned2017-05-09T01:17:41Z
    date available2017-05-09T01:17:41Z
    date issued2015
    identifier issn1528-8919
    identifier othergtp_137_04_041202.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/157908
    description abstractRain ingestion can significantly affect the performance and operability of gas turbine aeroengines. In order to study and understand rain ingestion phenomena at engine level, a performance model is required that integrates component models capable of simulating the physics of rain ingestion. The current work provides, for the first time in the open literature, information about the setup of a mixedfidelity engine model suitable for rain ingestion simulation and corresponding overall engine performance results. Such a model can initially support an analysis of rain ingestion during the predesign phase of engine development. Once components and engine models are validated and calibrated versus experimental data, they can then be used to support certification tests, the extrapolation of ground test results to altitude conditions, the evaluation of control or engine hardware improvements and eventually the investigation of inflight events. In the present paper, component models of various levels of fidelity are first described. These models account for the scoop effect at engine inlet, the fan effect and the effects of water presence in the operation and performance of the compressors and the combustor. Phenomena such as velocity slip between the liquid and gaseous phases, droplet breakup, droplet–surface interaction, droplet and film evaporation as well as compressor stages rematching due to evaporation are included in the calculations. Water ingestion influences the operation of the components and their matching, so in order to simulate rain ingestion at engine level, a suitable multifidelity engine model has been developed in the Proosis simulation platform. The engine model's architecture is discussed, and a generic high bypass turbofan is selected as a demonstration test case engine. The analysis of rain ingestion effects on engine performance and operability is performed for the worst case scenario, with respect to the water quantity entering the engine. The results indicate that rain ingestion has a strong negative effect on highpressure compressor surge margin, fuel consumption, and combustor efficiency, while more than half of the water entering the core is expected to remain unevaporated and reach the combustor in the form of film.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDevelopment and Integration of Rain Ingestion Effects in Engine Performance Simulations
    typeJournal Paper
    journal volume137
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4028545
    journal fristpage41202
    journal lastpage41202
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 004
    contenttypeFulltext
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