A Disk Rotating Detonation Engine Part 1:Design and Buildup (AIAA 2018-0633)
A Disk Rotating Detonation Engine Part 2: Operation (AIAA 2018-1607)
Characterizing Thermal Exit Conditions for an Ultra Compact Combustor (AIAA 2014-0456)
Chemiluminescence and High Speed Imaging of Reacting Film Cooling Layers
Comparison of In-Cylinder Pressure Measurement Methods in a Small Spark Ignition Engine
Design Strategy for Fuel Introduction to a Circumferential Combustion Cavity (AIAA 2018-1876)
Determination of Cooling Parameters for a High-Speed, True-Scale, Metallic Turbine Vane
Determination of Cooling Parameters for a High Speed, True Scale, Metallic Turbine Vane
Development of a Fiber-Optic PIV System for Turbomachinery Applications
Development of Test Bench and Characterization of Performance in Small Internal Combustion Engines
Dynamic Friction Measurements on a Small Engine Test Bench (AIAA 2015-1474)
Film Coolant Property Variation in Scaling Gas Turbine Cooling Effectiveness (AIAA 2016-0904)
Flame Structure Effects at High G-Loading
Heat Release in Turbine Cooling I: Experimental and Computational Comparison of Three Geometries
Increasing Reliability of a Two-Stroke Internal Combustion Engine for Dynamically Changing Altitudes
Increasing Reliability of a Two-Stroke Internal Combustion Engine for Dynamically Changing Altitudes
Investigation of In-Cylinder Pressure Measurement Methods within a Two-Stroke Spark Ignition Engine
Measurement of Loss Pathways in Small, Two-Stroke Internal-Combustion Engines
Measurements of Pressure and Temperature in a Short Duration Turbine Facility
Measuring Scaling Effects in Small Two-Stroke Internal Combustion Engines
Minimization of Heat Load Due to Secondary Reactions in Fuel Rich Environments
Mitigation of Heat Release from Film Cooling in Fuel-Rich Environments
Mitigation of Heat Release from Film Cooling in Fuel-Rich Environments
Mitigation of Heat Release from Film Cooling in Fuel-Rich Environments
Numerical Geometric Sensitivity Analysis Of Flow And Thermal Patterns Within A Combustor Simulator
Numerical Geometric Sensitivity Analysis Of Flow And Thermal Patterns Within A Combustor Simulator
Parameter Impact on Heat Flux in a Rotating Detonation Engine (AIAA 2018-0400)