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Flugtriebwerk
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Time-Varying Operating Condition–Based Prediction of the Remaining Useful Life for Aeroengine
NASA's X-57 High Lift Motor Controller: Detailed Design, Test Results, and Outcomes
Revolutionary Vertical Lift Technology Lift + Cruise Concept Vehicle Powertrain Dynamic Model
Fuel consumption estimation for jet aircraft: a mathematical model development
Hot Corrosion Damage Modeling in Aeroengines Based on Performance and Flight Mission
Aeroakustische Bewertung von Fanstufen im Rahmen des Vorentwurfs von Triebwerken
Exploring the possibilities of using bio-additives in military aviation fuels
Optimization of Lift-Plus-Cruise Vertical Take-Off and Landing Aircraft with Electrified Propulsion
Review of Contemporary Methods for Reliability Analysis in Aircraft Components
Evaluating an Additive Manufactured Acoustic Metamaterial Using the Advanced Noise Control Fan
Shock-Induced Separation and Control in a 4.32-Aspect-Ratio Test Section
SUbsonic Single Aft eNgine (SUSAN) Power/Propulsion System Control Architecture Updates
SUbsonic Single Aft eNgine (SUSAN) Power/Propulsion System Control Architecture Updates
Overview of NASA GRC Electrified Aircraft Propulsion (EAP) Controls Research
Overview of NASA GRC Electrified Aircraft Propulsion (EAP) Controls Research
Considering Turbofan Operability in Hybrid Electric Aircraft Propulsion System Design
Real-Time Hardware-in-the-Loop Evaluation of A Partially Turboelectric Propulsion Control Design
X-57 Electromagnetic Interference Design, Integration, and Test Consideration
Health Management Considerations for Electrified Aircraft Propulsion Systems
Health Management Considerations for Electrified Aircraft Propulsion Systems
Health Management Considerations for Electrified Aircraft Propulsion Systems
Review of the hybrid gas - electric aircraft propulsion systems versus alternative systems
NASA’s Quiet Electric ENgines (QUEEN): Summary of the QUEEN V2 Test
Market Analysis of the Subsonic Single Aft Engine (SUSAN) Transport Aircraft Concept
Real-time Hardware-in-the-Loop Evaluation of a Partially Turboelectric Propulsion Control Design
Real-Time Hardware-in-the-Loop Evaluation of A Partially Turboelectric Propulsion Control Design
Impedance Measurements of Motor Drives and Supplies in NASA NEAT Facility
Impedance Measurements of Motor Drives and Supplies in NASA NEAT Facility
Exploration of Design Drivers for the RVLT Lift+Cruise Reference Aircraft
X-57 High Lift Motor Controller Design and Testing
Scaling Electric Machines to a Megawatt and Material Options
Design Optimization of a Novel Boundary Layer Diverter for Semi-Submerged Inlets