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Flugtriebwerk
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Concepts for Variable/Multi-Speed Rotorcraft Drive System
Reestablishing Open Rotor as an Option for Significant Fuel Burn Improvements
Distributed Turboelectric Propulsion for Hybrid Wing Body Aircraft
Low-Enriched Uranium Nuclear Thermal Propulsion Systems
Multiplexed Predictive Control of a Large Commercial Turbofan Engine
Signal Detection Theory Applied to Helicopter Transmission Diagnostic Thresholds
Implementation of a Body Force Model into OVERFLOW for Propulsor Simulations
Conceptual Exploration of Aircraft Configurations for the SUSAN Electrofan
Water Injection on Commercial Aircraft to Reduce Airport Nitrogen Oxides
Low-Enriched Uranium Nuclear Thermal Propulsion Systems
Modeling and Control Design for a Turboelectric Single Aisle Aircraft Propulsion System
Advanced Powertrain Challenges for Turbo-electric/hybrid Electric Propulsion Applications
AQUIFER Review of AQUIFER Technology Feasibility June 15 -- 19, 2020
Comprehensive Validation of Skeletal Mechanism for Turbulent Premixed Methane–Air Flame Simulations
Initial Regulatory and Certification Approach for the SUSAN Electrofan Concept
Improving Engine Efficiency Through Core Developments
Turboelectric Distributed Propulsion in a Hybrid Wing Body Aircraft
X-57 Electromagnetic Interference Design, Integration, and Test Consideration
Health Management Considerations for Electrified Aircraft Propulsion Systems
NASA Meeting on Cryogenic Fuel Systems for Aircraft: Overview of Previous Workshops and Studies
Establishing Electrified Aircraft Propulsion Concepts
Update on SUSAN Concept Vehicle Power and Propulsion System
Review of the hybrid gas - electric aircraft propulsion systems versus alternative systems
Considering Turbofan Operability in Hybrid Electric Aircraft Propulsion System Design
Risk Reduction Testing of Superconducting Coils for the High Efficiency Megawatt Motor
Current Status and Future Plans for Electric Motors and Drives at NASA
The Design and Testing of a Miniature Turbofan Engine
Materials Aspects of Turboelectric Aircraft Propulsion
An Overview of Low-Emission Combustion Research at NASA Glenn
Overview of Engineering Design and Analysis at the NASA John C. Stennis Space Center
Hummingbird Hybrid - Micro Hybrid Electric Aircraft Propulsion System
Introduction to Advanced Engine Control Concepts
Adjoint-Based Minimization of X-59 Sonic Boom Noise Via Control Surfaces
An Experimental Approach to a Rapid Propulsion and Aeronautics Concepts Testbed
Investigation of Current Methods to Identify Helicopter Gear Health
The Case for Distributed Engine Control in Turbo-Shaft Engine Systems
Overview of NASA GRC Research on Damping of Jet Engine Blades