Pressure and fuel effects on turbulent consumption speeds of H2/CO blends

2013 ◽  
Vol 34 (1) ◽  
pp. 1527-1535 ◽  
Author(s):  
Prabhakar Venkateswaran ◽  
Andrew Marshall ◽  
Jerry Seitzman ◽  
Tim Lieuwen
Keyword(s):  
Fuel Effects

Comparison of Fuel Effects on Low Temperature Reactions in PPC and HCCI Combustion

2014 ◽  
Author(s):  
Hadeel Solaka Aronsson ◽  
Ida Truedsson ◽  
Martin Tuner ◽  
Bengt Johansson ◽  
William Cannella
Keyword(s):  
Low Temperature ◽  
Hcci Combustion ◽  
Fuel Effects

Measurement of Biodiesel Blend and Conventional Diesel Spray Structure Using X-Ray Radiography

2009 ◽  
Vol 131 (6) ◽  
Author(s):  
A. L. Kastengren ◽  
C. F. Powell ◽  
K.-S. Im ◽  
Y.-J. Wang ◽  
J. Wang
Keyword(s):  
Cone Angle ◽  
Injection Pressure ◽  
Fuel Distribution ◽  
X Ray ◽  
Spray Structure ◽  
Quantitative Measurements ◽  
Biodiesel Blend ◽  
Temporal And Spatial ◽  
Nozzle Geometries ◽  
Fuel Effects

The near-nozzle structure of several nonevaporating biodiesel-blend sprays has been studied using X-ray radiography. Radiography allows quantitative measurements of the fuel distribution in sprays to be made with high temporal and spatial resolution. Measurements have been made at different values of injection pressure, ambient density, and with two different nozzle geometries to understand the influences of these parameters on the spray structure of the biodiesel blend. These measurements have been compared with corresponding measurements of Viscor, a diesel calibration fluid, to demonstrate the fuel effects on the spray structure. Generally, the biodiesel-blend spray has a similar structure to the spray of Viscor. For the nonhydroground nozzle used in this study, the biodiesel-blend spray has a slightly slower penetration into the ambient gas than the Viscor spray. The cone angle of the biodiesel-blend spray is generally smaller than that of the Viscor spray, indicating that the biodiesel-blend spray is denser than the Viscor spray. For the hydroground nozzle, both fuels produce sprays with initially wide cone angles that transition to narrow sprays during the steady-state portion of the injection event. These variations in cone angle with time occur later for the biodiesel-blend spray than for the Viscor spray, indicating that the dynamics of the injector needle as it opens are somewhat different for the two fuels.

Fuel Effects on Diesel Emissions - A New Understanding

2001 ◽  
Author(s):  
Y Kwon ◽  
N Mann ◽  
D J Rickeard ◽  
R Haugland ◽  
Kjell Arne Ulvund ◽  
...  
Keyword(s):  
Diesel Emissions ◽  
Fuel Effects

scholarly journals Fuel Effects on the TF30 Engine (Alternate Test Procedure)

1984 ◽  
Author(s):  
P. A. Karpovich ◽  
A. I. Masters
Keyword(s):  
Test Procedure ◽  
Engine Performance ◽  
Combustion Efficiency ◽  
Fuel Properties ◽  
Secondary Importance ◽  
Turbine Engine ◽  
Main Burner ◽  
Alternate Test ◽  
Fuel Nozzle ◽  
Fuel Effects

The objective of the Alternate Test Procedure (ATP) is to develop the capability to qualify new fuels for Navy aircraft use with a minimum of testing. The effect of fuel composition and properties on engine performance and component life has been shown to vary significantly from one engine configuration to another. The P&WA approach to the ATP has been to define fuel effects on the TF30 engine and then apply the methodology to other engines of interest to the Navy. Investigations of the TF30 conducted under the ATP Program and other Navy and Air Force Contracts have produced one of the most complete fuel effect characterizations available for any gas turbine engine. Major fuel effects which have been quantified are the relationships of lubricity to main fuel control reliability, viscosity and volatility to main burner and augmentor ignition limits, and hydrogen content to smoke and combustor life. The effects of fuel properties and composition on combustion efficiency and elastomeric seal life were found to be of secondary importance. Remaining uncertainties are the effects of fuel properties on turbine life and fuel nozzle fouling rate.

Fuel Effects on the TF30 Engine (Alternate Test Procedure)

1985 ◽  
Vol 107 (3) ◽  
pp. 769-774
Author(s):  
P. A. Karpovich ◽  
A. I. Masters
Keyword(s):  
Test Procedure ◽  
Engine Performance ◽  
Combustion Efficiency ◽  
Fuel Properties ◽  
Secondary Importance ◽  
Turbine Engine ◽  
Main Burner ◽  
Alternate Test ◽  
Fuel Nozzle ◽  
Fuel Effects

The objective of the Alternate Test Procedure (ATP) is to develop the capability to qualify new fuels for Navy aircraft use with a minimum of testing. The effect of fuel composition and properties on engine performance and component life has been show to vary significantly from one engine configuration to another. The P&WA approach to the ATP has been to define fuel effects on the TF30 engine and then apply the methodology to other engines of interest to the Navy. Investigations of the TF30 conducted under the ATP Program and other Navy and Air Force Contracts have produced one of the most complete fuel effect characterizations available for any gas turbine engine. Major fuel effects which have been quantified are the relationships of lubricity to main fuel control reliability, viscosity and volatility to main burner and augmentor ignition limits, and hydrogen content to smoke and combustor life. The effects of fuel properties and composition on combustion efficiency and elastomeric seal life were found to be of secondary importance. Remaining uncertainties are the effects of fuel properties on turbine life and fuel nozzle fouling rate.

Temperature and fuel effects in sooting diffusion flames

1985 ◽  
Vol 20 (1) ◽  
pp. 1007-1015 ◽  
Author(s):  
J.H. Kent ◽  
H.Gg. Wagner
Keyword(s):  
Diffusion Flames ◽  
Fuel Effects
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