Andere Kunden interessierten sich auch für
![Mixing Effects of Pylon-Aided Fuel Injection Located Upstream of a Flameholding Cavity in Supersonic Flow]( "Mixing Effects of Pylon-Aided Fuel Injection Located Upstream of a Flameholding Cavity in Supersonic Flow")
Mixing Effects of Pylon-Aided Fuel Injection Located Upstream of a Flameholding Cavity in Supersonic Flow60,99 €![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 Flow60,99 €![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 Combustor60,99 €![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 Cavity60,99 €![Cavity Coupled Aeroramp Injector Combustion Study]( "Cavity Coupled Aeroramp Injector Combustion Study")
Cavity Coupled Aeroramp Injector Combustion Study60,99 €![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 Surrogaates60,99 €![A Computer Investigation of a Lobed-Mixer Fuel-Injection Strut in a Scramjet Engine Model]( "A Computer Investigation of a Lobed-Mixer Fuel-Injection Strut in a Scramjet Engine Model")
A Computer Investigation of a Lobed-Mixer Fuel-Injection Strut in a Scramjet Engine Model60,99 €
The Air Force Research Lab, Propulsion Directorate, Wright-Patterson Air Force Base, Ohio has studied several designs regarding cavity flameholding for supersonic RAMJET (SCRAMJET) applications. The most recent of these studies have concluded that direct injection of ethylene fuel into the aft cavity ramp produced an efficient, robust flameholder given specific freestream condition and fuel flow rate. The main goals of this experiment are: 1) study the effect on combustion of direct fuel and air injection in the main flameholding cavity and 2) characterization of the operational limits (i.e., sustained combustion limits) over a variety of fuel and air flow rates. Direct injection of both fuel and air provided additional capability to tune the cavity such that a more stable decentralized flame results. The addition of air injection provided the most improvement over the baseline case (fuel only) near the upstream portion of the cavity close to the cavity step.