Show simple item record

contributor authorFredrik Haglind
contributor authorRiti Singh
date accessioned2017-05-09T00:19:44Z
date available2017-05-09T00:19:44Z
date copyrightOctober, 2006
date issued2006
identifier issn1528-8919
identifier otherJETPEZ-26926#754_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133622
description abstractMainly owing to the dwindling fossil oil resources and the environmental concerns of discharging greenhouse gases into the atmosphere, it is essential to find an alternative to kerosene for civil aviation. This paper covers the main effects on aero engines when changing to hydrogen fuel. Particularly, emission and performance issues are discussed, but some design matters are also covered. By simply changing to hydrogen, small engine performance gains may be obtained. The results of the calculations suggest that there is the potential to design a combustion system using hydrogen that produces less NOx emissions than any system using kerosene.
publisherThe American Society of Mechanical Engineers (ASME)
titleDesign of Aero Gas Turbines Using Hydrogen
typeJournal Paper
journal volume128
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2179468
journal fristpage754
journal lastpage764
identifier eissn0742-4795
keywordsCombustion
keywordsFuels
keywordsEngines
keywordsCombustion chambers
keywordsDesign
keywordsTemperature
keywordsHydrogen
keywordsEmissions
keywordsHydrogen fuels
keywordsCooling
keywordsCycles AND Flames
treeJournal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 004
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record