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NASA Scientific and Technical Aerospace Reports - The University ...

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yet do show lower emissions. <strong>The</strong> evolution of a validated combustor design procedure is fundamental to the development of<br />

dynamic fueling of combustor systems for gas turbine engines that comply with multiple feedstock sources satisfying both new<br />

<strong>and</strong> legacy systems.<br />

Author<br />

Jet Engine Fuels; Performance Tests; Refueling; Combustion Chambers; Synthetic Fuels<br />

20100017283 <strong>NASA</strong> Glenn Research Center, Clevel<strong>and</strong>, OH, USA<br />

Particulate Emissions Hazards Associated with Fueling Heat Engines<br />

Hendricks, Robert C.; Bushnell, Dennis M.; [2010]; 8 pp.; In English; Original contains color illustrations<br />

Contract(s)/Grant(s): WBS 561581.02.08.03.16.03<br />

Report No.(s): ISROMAC13-2010-62; E-17207; No Copyright; Avail.: CASI: A02, Hardcopy<br />

ONLINE: http://hdl.h<strong>and</strong>le.net/2060/20100017283<br />

All hydrocarbon- (HC-) fueled heat engine exhaust (tailpipe) emissions (

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