Aircraft Technology Innovation

010

Aircraft Technology Modeling and Assessment

037

CLEEN II Technology Modeling and Assessment

047

Clean Sheet Supersonic Aircraft Engine Design and Performance

050

Over-Wing Engine Placement

051

Combustion Concepts for the Next-Generation Aircraft Engines

052

Comparative Assessment of Electrification Strategies for Aviation

055

Noise Generation and Propagation from Advanced Combustors

056

Turbine Cooling Through Additive Manufacturing

059

Jet Noise Modeling and Measurements to Support Reduced LTO Noise of Supersonic Aircraft Technology Development

063

Parametric Noise Modeling For Boundary Layer Ingesting Propulsors

064

Alternative Design Configurations to meet Future Demand

066

Evaluation of High Thermal Stability Fuels

067

Impact of Fuel Heating on Combustion and Emissions

068

Combustor Wall Cooling Concepts for Dirt Mitigation

070

Reduction of nvPM Emissions via Aero-Engine Fuel Injector Design

074

Low Emission Premixed Combustion Technology for Supersonic Civil Transport

075

Improved Engine Fan Broadband Noise Prediction Capabilities

076

Improved Open Rotor Noise Prediction Capabilities

077

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Aircraft Technology Innovation

Aircraft Technology Modeling and Assessment

CLEEN II Technology Modeling and Assessment

Clean Sheet Supersonic Aircraft Engine Design and Performance

Over-Wing Engine Placement

Combustion Concepts for the Next-Generation Aircraft Engines

Comparative Assessment of Electrification Strategies for Aviation

Noise Generation and Propagation from Advanced Combustors

Turbine Cooling Through Additive Manufacturing

Jet Noise Modeling and Measurements to Support Reduced LTO Noise of Supersonic Aircraft Technology Development

Parametric Noise Modeling For Boundary Layer Ingesting Propulsors

Alternative Design Configurations to meet Future Demand

Evaluation of High Thermal Stability Fuels

Impact of Fuel Heating on Combustion and Emissions

Combustor Wall Cooling Concepts for Dirt Mitigation

Reduction of nvPM Emissions via Aero-Engine Fuel Injector Design

Low Emission Premixed Combustion Technology for Supersonic Civil Transport

Improved Engine Fan Broadband Noise Prediction Capabilities

Improved Open Rotor Noise Prediction Capabilities

Measurements to Support Noise Certification for UAS/UAM Vehicles and Identify Noise Reduction Opportunities