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contributor authorYang, Bijie;Shu, Mengying;Martinez-Botas, Ricardo;Yang, Mingyang
date accessioned2022-12-27T23:22:52Z
date available2022-12-27T23:22:52Z
date copyright7/28/2022 12:00:00 AM
date issued2022
identifier issn0742-4795
identifier othergtp_144_09_091002.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4288517
description abstractThe turbocharged piston-driven engines are widely used in high altitude long endurance unmanned aerial vehicles (HALE UAVs). Repeated actions of engine pistons and valves give rise to engine pulsations resulting in intensive unsteady flows in the turbocharger. One-dimensional (1-D) modeling, which is computationally effective, plays a crucial role in evaluating turbocharger performance and conducting turbocharger-engine matching under pulsating conditions. The present work introduces a newly developed 1-D software (TURBODYNA) for the sake of improving traditional 1-D modeling's accuracy and generality. The advantages and capabilities of TURBODYNA are illustrated by applying it to three different and typical sorts of turbocharger applications: the single-entry turbine, the twin-entry turbine, and the centrifugal compressor. The unsteady testing conditions include high frequent pressure pulses for the single-entry turbine, out-of-phase pressure pulses for the twin-entry turbine, and rotating stall and surge for the centrifugal compressor. Results show that, by contrast to traditional 1-D modelings, the current 1-D modeling has achieved exceptional improvements in both accuracy and applicability. The novel and powerful tool provides a solid framework for assessing turbocharger unsteady performances and addressing turbocharger-engine matching.
publisherThe American Society of Mechanical Engineers (ASME)
titleTURBODYNA: A Generic One-Dimensional Dynamic Simulator for Radial Turbomachinery
typeJournal Paper
journal volume144
journal issue9
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4055018
journal fristpage91002
journal lastpage91002_10
page10
treeJournal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 009
contenttypeFulltext


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