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Mixing Effects of Pylon-Aided Fuel Injection Located Upstream of a Flameholding Cavity in Supersonic Flow59,99 €![An Experimental Investigation Studying the Influence of Dimples on a Film Cooled Turbine Blade Leading Edge]( "An Experimental Investigation Studying the Influence of Dimples on a Film Cooled Turbine Blade Leading Edge")
An Experimental Investigation Studying the Influence of Dimples on a Film Cooled Turbine Blade Leading Edge59,99 €![Fuel-Air Injection Effects on Combustion in Cavity-Based Flameholders in a Supersonic Flow]( "Fuel-Air Injection Effects on Combustion in Cavity-Based Flameholders in a Supersonic Flow")
Fuel-Air Injection Effects on Combustion in Cavity-Based Flameholders in a Supersonic Flow59,99 €![Performance Measurements of Direct Air Injection in a Cavity-Based Flameholder for a Supersonic Combustor]( "Performance Measurements of Direct Air Injection in a Cavity-Based Flameholder for a Supersonic Combustor")
Performance Measurements of Direct Air Injection in a Cavity-Based Flameholder for a Supersonic Combustor59,99 €![Critical Design Parameters for Pylon-Aided Gaseous Fuel Injection Upstream of a Flameholding Cavity]( "Critical Design Parameters for Pylon-Aided Gaseous Fuel Injection Upstream of a Flameholding Cavity")
Critical Design Parameters for Pylon-Aided Gaseous Fuel Injection Upstream of a Flameholding Cavity59,99 €![Effects of Jet Swirl on Mixing of a Light Gas Jet in a Supersonic Airstream]( "Effects of Jet Swirl on Mixing of a Light Gas Jet in a Supersonic Airstream")
Effects of Jet Swirl on Mixing of a Light Gas Jet in a Supersonic Airstream59,99 €![Characterization of Upstream Mixing Cavities and a Downstream Combustion Cavity in Supersonic Flow]( "Characterization of Upstream Mixing Cavities and a Downstream Combustion Cavity in Supersonic Flow")
Characterization of Upstream Mixing Cavities and a Downstream Combustion Cavity in Supersonic Flow59,99 €
In pursuit of a more efficient and effective fuel-air mixing for a SCRAM jet combustor, this study investigated relative near field effects of molecular weight on mixing and penetration of different gaseous injection into a supersonic (M=2.9) cross flow. Helium and argon gas were chosen as injectants because of the large differences in molecular weights. Also, mixing enhancement was observed by injecting the traverse gas jet parallel to the compression face of a ramp. Color schlieren photography was used to identify the shock structures and interactions in the flow field. Measurements of mean flow properties were used to establish the jet plume size, penetration, and concentration and to quantify the total pressure loss. Results indicate greater mixing and plume expansion can be achieved with helium compared to argon.