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A Survey of Current Rotorcraft Propulsion Health Monitoring Technologies
Developing Coatings and Disks with 1500 Degrees F Capability
High Temperature Investigations into an Active Turbine Blade Tip Clearance Control Concept
Jet-Surface Interaction Test: Phase 1 Results and Phase 2 Planning
Multiplexed Predictive Control of a Large Commercial Turbofan Engine
Signal Detection Theory Applied to Helicopter Transmission Diagnostic Thresholds
Effects of Gas Turbine Component Performance on Engine and Rotary Wing Vehicle Size and Performance
A Risk Assessment Architecture for Enhanced Engine Operation
Control Design for a Generic Commercial Aircraft Engine
A Comparison of Trajectory Refinement Schemes for GlennICE
NASA's Turbine Electrified Energy Management (TEEM) Control
NASA’s Electric Aircraft Propulsion Updates (Selected)
NASA / GE Aviation Collaborative Partnership Research in Ultra High Bypass Cycle Propulsion Concepts
Variable Noise Reduction Systems for a Notional Supersonic Business Jet
Implementation of a Body Force Model into OVERFLOW for Propulsor Simulations
Distributed Turboelectric Propulsion for Hybrid Wing Body Aircraft
Low-Enriched Uranium Nuclear Thermal Propulsion Systems
Integration Concept for a Hybrid-Electric Solid-Oxide Fuel Cell Power System into the X-57 "Maxwell"
Initial Regulatory and Certification Approach for the SUSAN Electrofan Concept
Review of the hybrid gas - electric aircraft propulsion systems versus alternative systems
X-57 Electromagnetic Interference Design, Integration, and Test Consideration
Implementation of Enhanced Propulsion Control Modes for Emergency Flight Operation
A Risk Management Architecture for Emergency Integrated Aircraft Control
Conceptual Exploration of Aircraft Configurations for the SUSAN Electrofan
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
Some Design Considerations for Two-Dimensional, Mixed-Compression Inlets for Mach 2.5 to 3.5
An Overview of Low-Emission Combustion Research at NASA Glenn
Investigation of Current Methods to Identify Helicopter Gear Health
Materials Aspects of Turboelectric Aircraft Propulsion
An Experimental Approach to a Rapid Propulsion and Aeronautics Concepts Testbed
Hypersonic Vehicle Propulsion System Simplified Model Development
Small UAV Research and Evolution in Long Endurance Electric Powered Vehicles
Supersonic Cruise Efficiency - Propulsion Tech Challenge Overview