Environmental particle rebound/deposition modeling in engine hot sections

نویسندگان

چکیده

The aircraft engine hot section is most vulnerable and failure prone to environmental particle ingestion, which, particularly for helicopters, can cause detrimental effects ranging from reduced performance complete failure. objective of this work develop an analytical tool assess impact on sections. current state the art in experimental research ingestion related sections was reviewed, with emphasis sand particles. From these efforts, available data model calibration were identified, innovative rebound/deposition has been developed. A semi-empirical approach selected particles bouncing off metal surfaces, where coefficients restitution measured a temperature range 297–1323 K are used calculate bounce-back velocity components. developed deposition based non-dimensional parameter analysis over more than seventy experiments surface temperature, one two critical parameters deposition, also included model. successfully implemented into commercial software checked step by step. It calibrated cases: [Arizona road dust (ARD)] impingement circular plate Mt. St. Helens volcanic ash impinging first-stage air-cooled nozzle guide vane (NGV). For former case, predicts fairly well variation rate flow/particle temperature. latter case indicates that at operating conditions be assessed Due lack would permit full calibration/validation, time being only under limited conditions. As additional relevant appears, will continuously improved.

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ژورنال

عنوان ژورنال: Frontiers in Mechanical Engineering

سال: 2023

ISSN: ['2297-3079']

DOI: https://doi.org/10.3389/fmech.2022.924755