Results 81 to 90 of about 22,653 (192)

Uniqueness of a Generalized Solution for a One-Dimensional Thermal Explosion Model of a Compressible Micropolar Real Gas

open access: yesMathematics
In 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
doaj   +1 more source

Effect of primary-zone equivalence ratio and hydrogen addition on exhaust emission in a hydrocarbon-fueled combustor [PDF]

open access: yes
The effects of reducing the primary-zone equivalence ratio on the exhaust emission levels of oxides of nitrogen, carbon monoxide, and unburned hydrocarbons in experimental hydrocarbon-fueled combustor segments at simulated supersonic cruise and idle ...
Ingebo, R. D., Norgren, C. T.
core   +1 more source

A steam inerting system for hydrogen disposal for the Vandenberg Shuttle [PDF]

open access: yes
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.
core   +1 more source

Gas sampling method for determining pollutant concentrations in the flame zone of two swirl-can combustor modules [PDF]

open access: yes
A gas sampling probe and traversing mechanism were developed to obtain detailed measurements of gaseous pollutant concentrations in the primary and mixing regions of combustors in order to better understand how pollutants are formed.
Duerr, R. A.
core   +1 more source

Performance and durability of improved air-atomizing splash-cone fuel nozzles [PDF]

open access: yes
An improved design of air-atomizing fuel nozzles was determined from a study of four differently shaped splash-cone fuel nozzles after 56 hr of durability testing in a combustor segment.
Ingebo, R. D., Norgren, C. T.
core   +1 more source

NASA/Pratt and Whitney experimental clean combustor program: Engine test results [PDF]

open access: yes, 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
core   +1 more source

Mechanism of methanol and formaldehyde emissions from methanol-fueled engines

open access: yesFuel Processing Technology
Methanol, 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
doaj   +1 more source

Gaseous exhaust emissions from a J-58 engine at simulated supersonic flight conditions [PDF]

open access: yes
Emissions of total oxides of nitrogen, unburned hydrocarbons, carbon monoxide, and carbon dioxide from a J-58 engine at simulated flight conditions of Mach 2.0, 2.4, and 2.8 at 19.8 km altitude are reported.
Holdeman, J. D.
core   +1 more source

Ignition of Deflagration and Detonation Ahead of the Flame due to Radiative Preheating of Suspended Micro Particles [PDF]

open access: yes, 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
core  

Numerical investigation on combustion performances of premixed H2-air jet flames above a sudden expansion micro-nozzle

open access: yesCase Studies in Thermal Engineering
Our previous study demonstrated that divergent micro-nozzles designed for H2-fueled domestic gas stoves can achieve a higher flame temperature than conventional straight micro-nozzles, but are more susceptible to flashback. To address this safety concern,
Bo Xu, Wanhao Liu, Aiwu Fan
doaj   +1 more source

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