MathematicsIn this paper, we analyze a quasi-linear parabolic initial-boundary problem describing the thermal explosion of a compressible micropolar real gas in one spatial dimension.
Angela Bašić-Šiško, Ivan Dražić
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Performance of a catalytic reactor at simulated gas turbine combustor operating conditions [PDF]
The performance of a catalytic reactor 12 cm in diameter and 17 cm long was evaluated at simulated gas turbine combustor operating conditions using premixed propane and air.
Anderson, D. N. +2 more
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Ignition of Deflagration and Detonation Ahead of the Flame due to Radiative Preheating of Suspended Micro Particles [PDF]
, 2015 We study a flame propagating in the gaseous combustible mixture with suspended inert particles. The gas is assumed to be transparent for the radiation emitted by the combustion products, while particles absorb and re-emit the radiation. Thermal radiation
Ivanov, M. F. +2 more
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The effect of water injection on nitric oxide emissions of a gas turbine combustor burning ASTM Jet-A fuel [PDF]
Tests were conducted to determine the effect of water injection on oxides of nitrogen (NOx) emissions of a full annular, ram induction gas turbine combustor burning ASTM Jet-A fuel.
Diehl, L. A. +2 more
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NASA/Pratt and Whitney experimental clean combustor program: Engine test results [PDF]
, 1977 A two-stage vorbix (vortex burning and mixing) combustor and associated fuel system components were successfully tested in an experimental JT9D engine at steady-state and transient operating conditions, using ASTM Jet-A fuel. Full-scale JT9D experimental
Fiorentino, A. J. +2 more
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Gaseous exhaust emissions from a JT8D-109 turbofan engine at simulated cruise flight conditions [PDF]
Gaseous emissions from a JT8D-109 turbofan engine were measured in an altitude facility at four simulated cruise flight conditions: Mach 0.8 at altitudes of 9.1, 10, 7, and 12.2 km and Mach 0.9 at 10.7 km.
Diehl, L. A., Holdeman, J. D.
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Parametric performance of a turbojet engine combustor using jet A and A diesel fuel [PDF]
The performance of a single-can JT8D combustor was evaluated with Jet A and a high-aromatic diesel fuel over a parametric range of combustor-inlet conditions.
Butze, H. F., Humenik, F. M.
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Reverse-flow combustor for small gas turbines with pressure-atomizing fuel injectors [PDF]
A reverse flow combustor suitable for a small gas turbine (2 to 3 kg/s mass flow) was used to evalute the effect of pressure atomizing fuel injectors on combustor performance.
Mularz, E. J. +2 more
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A steam inerting system for hydrogen disposal for the Vandenberg Shuttle [PDF]
A two-year feasibility and test program to solve the problem of unburned confined hydrogen at the Vandenberg Space Launch Complex Six (SLC-6) during Space Shuttle Main Engine (SSME) firings is discussed.
Belknap, Stuart B.
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Mechanism of methanol and formaldehyde emissions from methanol-fueled engines
Fuel Processing TechnologyMethanol, as a low-carbon fuel, has broad application prospects in engines. The mechanism of methanol and formaldehyde was investigated respectively in a methanol premixed combustion test bench (PCTB) and a 304 stainless-steel flow reactor (SFR).
Fangjie Liu +4 more
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