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Overview of NASA GRC Electrified Aircraft Propulsion (EAP) Controls Research
System-Level Control Concepts for Electrified Aircraft Propulsion Systems
System-Level Control Concepts for Electrified Aircraft Propulsion Systems
Real-Time Hardware-in-the-Loop Evaluation of A Partially Turboelectric Propulsion Control Design
Feasibility of Electrified Propulsion for Ultra-Efficient Commercial Aircraft Final Report
Implementation Approach for an Electrified Aircraft Concept Vehicle in a Research Flight Simulator
Aircraft Engine Technology for Green Aviation to Reduce Fuel Burn
Investigation of "6X" Scramjet Inlet Configurations
Implementation of an Integrated On-Board Aircraft Engine Diagnostic Architecture
Aircraft Turbine Engine Control Research at NASA Glenn Research Center
Flight Simulator Evaluation of Enhanced Propulsion Control Modes for Emergency Operation
A Survey of Current Rotorcraft Propulsion Health Monitoring Technologies
Performance and Weight Estimates for an Advanced Open Rotor Engine
A Multidisciplinary Approach to Mixer-Ejector Analysis and Design
Computational Analysis of a Low-Boom Supersonic Inlet
Overview of Propulsion Controls and Diagnostics Research at NASA Glenn
The Effect of Faster Engine Response on the Lateral Directional Control of a Damaged Aircraft
Nonlinear Dynamic Modeling and Controls Development for Supersonic Propulsion System Research
Review of Propulsion Technologies for N+3 Subsonic Vehicle Concepts
Effects of Gas Turbine Component Performance on Engine and Rotary Wing Vehicle Size and Performance
Control Design for a Generic Commercial Aircraft Engine
2011-2012 Dryden Center Innovation Fund End of the Year Report: Altitude-Compensating Rocket Nozzles
A Risk Management Architecture for Emergency Integrated Aircraft Control
NASA Glenn's Contributions to Aircraft Engine Noise Research
Gas Turbine Characteristics for a Large Civil Tilt-Rotor (LCTR)
Health Management Considerations for Electrified Aircraft Propulsion Systems
Health Management Considerations for Electrified Aircraft Propulsion Systems
Health Management Considerations for Electrified Aircraft Propulsion Systems
Control Activity in Support of NASA Turbine Based Combined Cycle (TBCC) Research
Axisymmetric Calculations of a Low-Boom Inlet in a Supersonic Wind Tunnel
Propulsion Investigation for Zero and Near-Zero Emissions Aircraft
NASA’s Quiet Electric ENgines (QUEEN): Summary of the QUEEN V2 Test
Signal Detection Theory Applied to Helicopter Transmission Diagnostic Thresholds
Automated Power Assessment for Helicopter Turboshaft Engines
Concepts for Variable/Multi-Speed Rotorcraft Drive System
An Experimental Approach to a Rapid Propulsion and Aeronautics Concepts Testbed
Investigation of Current Methods to Identify Helicopter Gear Health