The Initial Design of a Fluidically-controlled Variable Geometry Fuel Injector PDF Download

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The Initial Design of a Fluidically-controlled Variable Geometry Fuel Injector

The Initial Design of a Fluidically-controlled Variable Geometry Fuel Injector PDF Author: K. D. Brundish
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


The Initial Design of a Fluidically-controlled Variable Geometry Fuel Injector

The Initial Design of a Fluidically-controlled Variable Geometry Fuel Injector PDF Author: K. D. Brundish
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


Design, Modeling, and Control of a Variable Geometry Spray Fuel Injector

Design, Modeling, and Control of a Variable Geometry Spray Fuel Injector PDF Author: John Paul Lien
Publisher:
ISBN:
Category :
Languages : en
Pages : 133

Book Description


Initial Optimisation of a Fluidically-controlled Variable Swirl Fuel Injector

Initial Optimisation of a Fluidically-controlled Variable Swirl Fuel Injector PDF Author: K. D. Brundish
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 548

Book Description


Gas Turbine Pollutant Emissions

Gas Turbine Pollutant Emissions PDF Author: IMechE (Institution of Mechanical Engineers)
Publisher: Wiley
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 120

Book Description
The latest data on air traffic's effect on climate change and air quality Air traffic emissions are a concern that will only grow as the volume of air traffic continues to increase; from reducing air quality in residential areas to contributing to climate change, these concerns are thus far only addressed in the lab. Gas Turbine Pollutant Emissions provides a comprehensive overview of the situation and offers direction for work focusing on application. Emphasizing the net global warming effects of oxides and contrails generated at altitude, this book offers particular insight for those working on low-emission and fuel-efficient technologies.

35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 560

Book Description


Design of a Fluidic-controlled Fuel-injector System for an Internal Combustion Engine

Design of a Fluidic-controlled Fuel-injector System for an Internal Combustion Engine PDF Author: George Wayne Hawkins
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

Book Description


Multi-objective Design Optimization of a Variable Geometry Spray Fuel Injector

Multi-objective Design Optimization of a Variable Geometry Spray Fuel Injector PDF Author: John Richard Archer
Publisher:
ISBN:
Category :
Languages : en
Pages : 35

Book Description


ASME Technical Papers

ASME Technical Papers PDF Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 482

Book Description


Design of a Liquid Fuel Injector for Alternative Fuel Studies in an Atmospheric Model Gas Turbine Combustor

Design of a Liquid Fuel Injector for Alternative Fuel Studies in an Atmospheric Model Gas Turbine Combustor PDF Author: John Ernest Stevenson
Publisher:
ISBN:
Category : Fuel
Languages : en
Pages : 54

Book Description
A new liquid-fuel injector was designed for use in the atmospheric-pressure, model gas turbine combustor in Bucknell University's Combustion Research Laboratory during alternative fuel testing. The current liquid-fuel injector requires a higher-than-desired pressure drop and volumetric flow rate to provide proper atomization of liquid fuels. An air-blast atomizer type of fuel injector was chosen and an experiment utilizing water as the working fluid was performed on a variable-geometry prototype. Visualization of the spray pattern was achieved through photography and the pressure drop was measured as a function of the required operating parameters. Experimental correlations were used to estimate droplet sizes over flow conditions similar to that which would be experienced in the actual combustor. The results of this experiment were used to select the desired geometric parameters for the proposed final injector design and a CAD model was generated. Eventually, the new injector will be fabricated and tested to provide final validation of the design prior to use in the combustion test apparatus.