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An Overview of Low-Emission Combustion Research at NASA Glenn
Investigation of Current Methods to Identify Helicopter Gear Health
Materials Aspects of Turboelectric Aircraft Propulsion
An Experimental Approach to a Rapid Propulsion and Aeronautics Concepts Testbed
Hypersonic Vehicle Propulsion System Simplified Model Development
Small UAV Research and Evolution in Long Endurance Electric Powered Vehicles
Supersonic Cruise Efficiency - Propulsion Tech Challenge Overview
Overview of Engineering Design and Analysis at the NASA John C. Stennis Space Center
Expansion of nickel-based alloy and specialty alloy capabilities
System Analysis and Performance Benefits of an Optimized Rotorcraft Propulsion System
The Design and Testing of a Miniature Turbofan Engine
A Cryogenically-Cooled MW Inverter for Electric Aircraft Propulsion
Green Propulsion Technologies for Advanced Air Transports
Ceramic Matrix Composites for Rotorcraft Engines
Comprehensive Validation of Skeletal Mechanism for Turbulent Premixed Methane–Air Flame Simulations
Aqueous, Quick-Charging Battery Integration for Electric Flight Research (AQUIFER)
Nitric Oxide PLIF Visualization of Simulated Fuel-Air Mixing in a Dual-Mode Scramjet
Preliminary Design of the Superconducting Rotor for NASA's High-Efficiency Megawatt Motor
Turbofan Engine Core Compartment Vent Aerodynamic Configuration Development Methodology
Engine Company Evaluation of Feasibility of Aircraft Retrofit Water-Injected Turbomachines
Thermal Hydraulics for Nuclear Space Applications
Major expansion of titanium capabilities
Grinding technology streamlines manufacture of jet engine compressor blades
Propulsion Controls Modeling for a Small Turbofan Engine
Rate-Based Model Predictive Control of Turbofan Engine Clearance
Evaluation of an Outer Loop Retrofit Architecture for Intelligent Turbofan Engine Thrust Control
Fluidic Oscillator Array for Synchronized Oscillating Jet Generation
Test Rig for Active Turbine Blade Tip Clearance Control Concepts: An Update
Automated Power Assessment for Helicopter Turboshaft Engines
Preparations for Tomographic Background-Oriented Schlieren at the 31-Inch Mach 10 Wind Tunnel
Markov Nonlinear System Estimation for Engine Performance Tracking
Some Design Considerations for Two-Dimensional, Mixed-Compression Inlets for Mach 2.5 to 3.5.
Rotorcraft Health Management Issues and Challenges