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Flugtriebwerk
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Modeling and Control Design for a Turboelectric Single Aisle Aircraft Propulsion System
Improving Engine Efficiency Through Core Developments
Turboelectric Distributed Propulsion in a Hybrid Wing Body Aircraft
Aero-Propulsion Control Research in Support of NASA Aeronautics Research Strategic Thrusts
Axisymmetric Calculations of a Low-Boom Inlet in a Supersonic Wind Tunnel
Computational Analysis of a Low-Boom Supersonic Inlet
Determining the Pressure Gain of Pressure Gain Combustion
Review of Propulsion Technologies for N+3 Subsonic Vehicle Concepts
Propulsion Technologies for Future Commercial Aircraft
Advanced Concepts for Aircraft LTO NOx Reduction: A NASA Perspective
Assessment of Turbulence-Chemistry Interaction Models in the National Combustion Code (NCC) - Part I
LEAPTech/HEIST Experiment Test and Evaluations Lessons Learned
Liquefied Bleed for Stability and Efficiency of High Speed Inlets
Reestablishing Open Rotor as an Option for Significant Fuel Burn Improvements
LEAPTech/HEIST Experiment Test and Evaluation Summary
Design of a High Power Density, High Efficiency, Low THD 250kW Converter for Electric Aircraft
Adjoint-Based Minimization of X-59 Sonic Boom Noise Via Control Surfaces
The Power for Flight: NASA's Contributions to Aircraft Propulsion
The Electrifying Future of Air Transportation
The Electrifying Future of Air Transportation
The NASA Environmentally Responsible Aviation Project/General Electric Open Rotor Test Campaign
NASA Glenn's Contributions to Aircraft Engine Noise Research
Coupled Aeropropulsive Design Optimization of a Podded Electric Propulsor
Water Injection on Commercial Aircraft to Reduce Airport Nitrogen Oxides
Comparison of an Inductance In-Line Oil Debris Sensor and Magnetic Plug Oil Debris Sensor
Progress Towards the Aerodynamic Testing of the High Efficiency Centrifugal Compressor
Investigation of "6X" Scramjet Inlet Configurations
Gas Turbine Characteristics for a Large Civil Tilt-Rotor (LCTR)
Control Activity in Support of NASA Turbine Based Combined Cycle (TBCC) Research
Summary of the Large Civil Tiltrotor (LCTR2) Engine Gearbox Study
Correlate Life Predictions and Condition Indicators in Helicopter Tail Gearbox Bearings
The History and Promise of Combined Cycle Engines for Access to Space Applications
Coaxial Propellant Injectors With Faceplate Annulus Control
Revolutionary Vertical Lift Technology (RVLT) Electric Propulsion
Volume Dynamics Propulsion System Modeling for Supersonics Vehicle Research
Current Status and Future Plans for Electric Motors and Drives at NASA