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contributor authorPezhman Akbari
contributor authorRazi Nalim
contributor authorNorbert Müller
date accessioned2017-05-09T00:19:58Z
date available2017-05-09T00:19:58Z
date copyrightJanuary, 2006
date issued2006
identifier issn1528-8919
identifier otherJETPEZ-26894#190_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133736
description abstractSignificant performance enhancement of microturbines is predicted by implementing various wave-rotor-topping cycles. Five different advantageous cases are considered for implementation of a four-port wave rotor into two given baseline engines. In these thermodynamic analyses, the compressor and turbine pressure ratios and the turbine inlet temperatures are varied, according to the anticipated design objectives of the cases. Advantages and disadvantages are discussed. Comparison between the theoretic performance of wave-rotor-topped and baseline engines shows a performance enhancement up to 34%. General design maps are generated for the small gas turbines, showing the design space and optima for baseline and topped engines. Also, the impact of ambient temperature on the performance of both baseline and topped engines is investigated. It is shown that the wave-rotor-topped engines are less prone to performance degradation under hot-weather conditions than the baseline engines.
publisherThe American Society of Mechanical Engineers (ASME)
titlePerformance Enhancement of Microturbine Engines Topped With Wave Rotors
typeJournal Paper
journal volume128
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1924484
journal fristpage190
journal lastpage202
identifier eissn0742-4795
keywordsEngines
keywordsCompressors
keywordsWaves
keywordsRotors
keywordsPressure
keywordsTemperature AND Turbines
treeJournal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 001
contenttypeFulltext


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