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Flugtriebwerk
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Rotorcraft Health Management Issues and Challenges
Multipurpose Rotating Rake Arrays for Integrated Inlet and Fan Stage Performance Measurement
Subsonic Single Aft Engine (SUSAN) Transport Aircraft Concept and Trade Space Exploration
NASA’s Quiet Electric ENgines (QUEEN): Summary of the QUEEN V2 Test
Supersonic External-Compression Inlets for Mach 1.4 to 2.0
NASA Reference Motor Designs for Electric Vertical Takeoff and Landing Vehicles
Overview of Low Emission Combustion Research At NASA Glenn
Revolutionary Vertical Lift Technology (Rvlt) Side-By-Side Hybrid Powertrain Dynamic Model
Update on Subsonic Single Aft Engine (SUSAN) Electrofan Trade Space Exploration
Cooling of Electric Motors Used for Propulsion on SCEPTOR
Low-Speed Active Flow Control Laboratory Developed
Intelligent Engine Systems Work Element 1.2: Malfunction and Operator Error Reduction
NASA Glenn Research in Controls and Diagnostics for Intelligent Aerospace Propulsion Systems
Liquid-Hydrogen-Cooled 450-hp Electric Motor Test Stand Being Developed
High-Altitude, Long-Endurance Airships for Coastal Surveillance
Oil-Free Rotor Support Technologies for an Optimized Helicopter Propulsion System
Market Analysis of the Subsonic Single Aft Engine (SUSAN) Transport Aircraft Concept
Numerical Simulation of the RTA Combustion Rig
X-57 Flight Performance and Failure Considerations
High-Temperature (1000 F) Magnetic Thrust Bearing Test Rig Completed and Operational
Water Injection Feasibility for Boeing 747 Aircraft
A Comparative Propulsion System Analysis for the High-Speed Civil Transport
Damage-Tolerant, Affordable Composite Engine Cases Designed and Fabricated
The X-43A Flight Research Program: Lessons Learned on the Road to Mach 10
Local Flow Conditions for Propulsion Experiments on the NASA F-15B Propulsion Flight Test Fixture
Towards an Aero-Propulso-Servo-Elasticity Analysis of a Commercial Supersonic Transport
Electric Motors for Non-Cryogenic Hybrid Electric and Turboelectric Propulsion
Analysis and Design of Rectangular-Cross-Section Nozzles for Scramjet Engine Testing
Critical Low-Noise Technologies Being Developed for Engine Noise Reduction Systems Subproject
ADAPTIVE CLEARANCE CONTROL SYSTEMS FOR TURBINE ENGINES
Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements