Results 81 to 90 of about 92,929 (279)
Experimental clean combustor program, alternate fuels addendum, phase 2 [PDF]
The characteristics of current and advanced low-emissions combustors when operated with special test fuels simulating broader range combustion properties of petroleum or coal derived fuels were studied.
Bahr, D. W., Gleason, C. C.
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Emissions control for ground power gas turbines [PDF]
, 1977 The similarities and differences of emissions reduction technology for aircraft and ground power gas turbines is described. The capability of this technology to reduce ground power emissions to meet existing and proposed emissions standards is presented ...
Anderson, D. N. +5 more
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European Journal of Inorganic Chemistry, Volume 28, Issue 30, October 22, 2025.As the reduction of transition metal oxides by coal poses a significant climate risk, the use of alternative reducing agents such as hydrogen is becoming increasingly important. This review summarizes the current knowledge of the reduction pathways of transition metal oxides from groups 6 to 8.
Michael Häger +2 more
wiley +1 more source
Polish Maritime ResearchThis work presents a 3D numerical study of a steam-injected combustor for a gas turbine operating on an ammonia-hydrogen fuel blend, aimed at enabling carbon-free hybrid energy systems. The research focuses on the performance and emission characteristics
Serbin Serhiy +4 more
doaj +1 more source
Polish Maritime Research, 2019 In this paper, we consider the issue of thermo-chemical heat recovery of waste heat from gas turbine engines for the steam conversion of associated gas for offshore vessels. Current trends in the development of offshore infrastructure are identified, and
Cherednichenko Oleksandr +2 more
doaj +1 more source
Combustor fluctuating pressure measurements in engine and in a component test facility: A preliminary comparison [PDF]
In a program to investigate combustor noise, measurements were made with a YF-102 engine of combustor internal fluctuating pressure and far field noise. The relationship of far field noise to engine internal measurement was ascertained. The relationships
Karchmer, A., Reshotko, M.
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Swirl can primary combustor [PDF]
, 1973 A swirl can full annulus combustor, operable over a wide range of exit average temperatures is used in a high performance gas turbine engine for advanced aircraft.
Jones, R. E., Niedzwiecki, R. W.
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Performance Analysis of Pulse Detonation Micro Gas Turbines Under Typical Operating Conditions
Energy Science &Engineering, Volume 13, Issue 10, Page 4690-4703, October 2025.ABSTRACT Considering the benefits of pulse detonation combustion, including low entropy increase, high cycle thermal efficiency, and self‐pressurization, a performance calculation model for a pulse detonation micro gas turbine was established using methane as fuel. The study primarily investigated the impact of component parameters, ambient conditions,
Weifeng Qin +3 more
wiley +1 more source
Experimental clean combustor program; noise measurement addendum, Phase 2 [PDF]
Combustor noise measurements were performed using wave guide probes. Test results from two full scale annular combustor configurations in a combustor test rig are presented.
Bekofske, K. L., Emmerling, J. J.
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Hypersonic research engine project. Phase 2: Some combustor test results of NASA aerothermodynamic integration model [PDF]
Combustor test results of the NASA Aerothermodynamic Integration Model are presented of a ramjet engine developed for operation between Mach 3 and 8.
Gaede, A. E., Sainio, W. C., Sun, Y. H.
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