Impact of IPS and IRS Configuration on Engine Installation Design
Application Layer—Generator Sets and Industrial
Distortion Tolerant Control Demonstrated in Flight
NASA N3-X with Turboelectric Distributed Propulsion
Middleware Service for the Integration of Control Systems of the Aviation Engine and Aircraft
NASA-JAXA Joint Management Approach for Upper Stage Engine System Development
Low-Order Parametric Analysis of a Rotating Detonation Engine in Rocket Mode
NASA Electrified Propulsion Research Summary
Aircraft Noise Reduction Subproject Overview
Study on Close Air Support System Based on Information Integration
Aircraft Gas Turbine Engine Health Management System Development and Integration Guide
Near-Optimal Feedback Strategies Synthesized Using a Spatial Statistical Approach
Concurrent Optimization of Airframe and Engine Design Parameters
Low Noise Cruise Efficient Short Take-Off and Landing Transport Vehicle Study
Engine Conceptual Design Studies for a Hybrid Wing Body Aircraft