Results 131 to 140 of about 21,213 (234)

Fuel Effects on Aviation Engine Emissions: A Chemical Reactor Network Modeling Study. [PDF]

Energy Fuels
Lopez-Pintor D, MacDonald J, Ramirez-Correa E, Garcia-Oliver JM, Payri R, Marti Gomez-Aldaravi P, Leyland P.   +6 more
europepmc   +1 more source

Substantial aircraft contrail formation at low soot emission levels. [PDF]

Nature
Voigt C, Märkl R, Sauer D, Dischl R, Renard C, Seeliger K, Yu F, Kaufmann S, Bräuer T, Jurkat-Witschas T, Le Chenadec G, Moreau J, Requena-Esteban E, Bonne N, Vals M, Roche A, Zelina J, Dörnbrack A, Eirenschmalz L, Heckl C, Horst E, Lichtenstern M, Marsing A, Neumann G, Roiger A, Scheibe M, Stock P, Giez A, Eckel G, Le Clercq P.   +29 more
europepmc   +1 more source

Investigation of Vaporized Kerosene Injection in a Supersonic Model Combustor

, 2003
Characteristics of vaporized aviation kerosene injection in a supersonic model combustor were preliminarily investigated. The electrically storage type heater has a volume capacity of heating kerosene of 0.8 kg up to 670 K at a pressure of 5.5 Mpa.
Li JG(李建国), Yu G(俞刚), 俞刚, Zhang XY(张新宇), Zhao Z, Sun CJ   +5 more
core  

Optimization strut-based fuel injection using multi-step hydrogen jets and air-assisted mixing in supersonic flow. [PDF]

Sci Rep
Houria ZB, Hajlaoui K, Aminian SA, Musa VA, Sadeq AM, Shaban M, Aich W, Kriaa K.   +7 more
europepmc   +1 more source

Performance of a Supersonic Model Combustor using Vaporized Kerosene Injection

, 2004
Characteristics of supersonic combustion by injecting kerosene vapor into a Mach 2.5 crossflow at various preheat temperatures and pressures were investigated experimentally.
Sun ZR(孙知人), Li JG(李建国), Yu G(俞刚), Zhang XY(张新宇), Fan XJ(范学军), 范学军   +5 more
core  

Temporally resolved planar measurements of transient phenomena in a partially pre-mixed swirl flame in a gas turbine model combustor

, 2010
Carter, Campbell, Meier, Wolfgang, Boxx, Isaac   +2 more
core   +1 more source

Clean catalytic combustor program

, 1983
A combustor program was conducted to evolve and to identify the technology needed for, and to establish the credibility of, using combustors with catalytic reactors in modern high-pressure-ratio aircraft turbine engines.
Lyon, T. F., Sabla, P. E., Dodds, W. J., Ekstedt, E. E.   +3 more
core  

Optimized steam boiler for soil steam disinfection: Structural design, CFD simulation, and field application. [PDF]

PLoS One
Pan S.
europepmc   +1 more source

Pareto-based design of thermophotovoltaic micro-combustors via a novel framework combining IGWO-tuned ANN, multi-objective multi-verse optimization, and ARAS-based decision making. [PDF]

Sci Rep
Alawad MA, Omar I, Alizadeh A, Shaban M, Sadeq AM, Singh Sawaran Singh N, Louhichi B, Mostafa L.   +7 more
europepmc   +1 more source

Transient catalytic combustor model

, 1981
A quasi-steady gas phase and thermally thin substrate model is used to analyze the transient behavior of catalytic monolith combustors in fuel lean operation. The combustor response delay is due to the substrate thermal inertia.
Tien, J. S.
core