Low-emissions gas turbine combustor development using sector and full annular rigs-Reference-Cited by-同舟云学术

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Low-emissions gas turbine combustor development using sector and full annular rigs

Published:1998-07-13 Issue: Volume: Page:
ISSN:
Container-title:34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Zelina J.¹,Cardenas M.¹,Tomondi C.¹,Penko P.²

Affiliation:

1. AlliedSignal Engines, Phoenix, AZ

2. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3528

Reference8 articles.

1. Brehm, N., Baker, S. J., Jones, S. P., 1997, "A Three Step NOXReduction Programme: Acheivements with the Single Annular Low-NOxCombustor for the BR 700 EngineFamily,"ASME97-GT-145.

2. Fuel effects on gas turbine combustion-liner temperature, pattern factor, and pollutant emissions

3. Zeldovich, Y., B., 1946,Acta Physeochem USSR 21,557.

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