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Flugtriebwerk
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Propulsion Technologies for Future Aircraft Generations: Clean, Lean, Quiet, and Green
The Promise and Challenges of Ultra High Bypass Ratio Engine Technology and Integration
Control Activity in Support of NASA Turbine Based Combined Cycle (TBCC) Research
Summary of the Large Civil Tiltrotor (LCTR2) Engine Gearbox Study
Noise from Aft Deck Exhaust Nozzles: Differences in Experimental Embodiments
The Electrifying Future of Air Transportation
A Comparison of Trajectory Refinement Schemes for GlennICE
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
Volume Dynamics Propulsion System Modeling for Supersonics Vehicle Research
Nonlinear Dynamic Modeling and Controls Development for Supersonic Propulsion System Research
Axisymmetric Calculations of a Low-Boom Inlet in a Supersonic Wind Tunnel
Integration Concept for a Hybrid-Electric Solid-Oxide Fuel Cell Power System into the X-57 "Maxwell"
Developing Coatings and Disks with 1500 Degrees F Capability
Implementation of Enhanced Propulsion Control Modes for Emergency Flight Operation
A Risk Management Architecture for Emergency Integrated Aircraft Control
Modeling and Control Design for a Turboelectric Single Aisle Aircraft Propulsion System
Coaxial Propellant Injectors With Faceplate Annulus Control
Coupled Aeropropulsive Design Optimization of a Podded Electric Propulsor
Multiplexed Predictive Control of a Large Commercial Turbofan Engine
Signal Detection Theory Applied to Helicopter Transmission Diagnostic Thresholds
Jet-Surface Interaction Test: Phase 1 Results and Phase 2 Planning
Improving Engine Efficiency Through Core Developments
Turboelectric Distributed Propulsion in a Hybrid Wing Body Aircraft
NASA Glenn's Contributions to Aircraft Engine Noise Research
NASA's Turbine Electrified Energy Management (TEEM) Control
NASA’s Electric Aircraft Propulsion Updates (Selected)
Gas Turbine Characteristics for a Large Civil Tilt-Rotor (LCTR)
LEAPTech/HEIST Experiment Test and Evaluation Summary
Implementation of a Body Force Model into OVERFLOW for Propulsor Simulations
Reestablishing Open Rotor as an Option for Significant Fuel Burn Improvements
Materials Aspects of Turboelectric Aircraft Propulsion
Water Injection on Commercial Aircraft to Reduce Airport Nitrogen Oxides
Initial Regulatory and Certification Approach for the SUSAN Electrofan Concept