Andere Kunden interessierten sich auch für
![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 Cavity56,99 €![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 €![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 €![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 Combustor58,99 €![Experimental Investigation of the Influence of Molecular Weight on Mixing and Penetration in Supersonic Dissimilar Gaseous Injection Into a Supersonic]( "Experimental Investigation of the Influence of Molecular Weight on Mixing and Penetration in Supersonic Dissimilar Gaseous Injection Into a Supersonic")
Experimental Investigation of the Influence of Molecular Weight on Mixing and Penetration in Supersonic Dissimilar Gaseous Injection Into a Supersonic59,99 €![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 Airstream58,99 €![Scramjet Fuel Injection Array Optimization Utilizing Mixed Variable Pattern Search with Kriging Surrogaates]( "Scramjet Fuel Injection Array Optimization Utilizing Mixed Variable Pattern Search with Kriging Surrogaates")
Scramjet Fuel Injection Array Optimization Utilizing Mixed Variable Pattern Search with Kriging Surrogaates59,99 €
The Air Force Research Lab (AFRL), Propulsion Directorate, Wright-Patterson Air Force Base, Ohio is conducting ongoing research into propulsive efficiency in supersonic ramjet (scramjet) technology. One current focus of this research is the usefulness of flameholding cavities implemented in the supersonic hydrocarbon-fueled combustion chamber. Because good mixing and proper cavity-core interaction lead to more efficient combustion, methods of optimizing fuel/air mixing both within and upstream the cavity are investigated. In a cooperative effort with the Air Force Institute of Technology (AFIT), AFRL provided a supersonic wind tunnel outfitted with an existing cavity design.