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Flugtriebwerk
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Modeling Turboshaft Engines for the Revolutionary Vertical Lift Technology Project
Modeling Turboshaft Engines for the Revolutionary Vertical Lift Technology Project
Low-Noise Operating Mode for Propeller-Driven Electric Airplanes
Advanced Single-Aisle Transport Propulsion Design Options Revisited
Gas Turbine Characteristics for a Large Civil Tilt-Rotor (LCTR)
Summary of the Large Civil Tiltrotor (LCTR2) Engine Gearbox Study
Propulsion Investigation for Zero and Near-Zero Emissions Aircraft
Analysis of Turbofan Design Options for an Advanced Single-Aisle Transport Aircraft
Effects of Gas Turbine Component Performance on Engine and Rotary Wing Vehicle Size and Performance
A Comparative Propulsion System Analysis for the High-Speed Civil Transport
A Noise and Emissions Assessment of the N3-X Transport
Electrical Systems Analysis at NASA Glenn Research Center: Status and Prospects
Design Study of Propulsion and Drive Systems for the Large Civil TiltRotor (LCTR2) Rotorcraft
Noise-Reduction Benefits Analyzed for Over-the-Wing-Mounted Advanced Turbofan Engines
Updated Assessment of an Open Rotor Airplane Using an Advanced Blade Design
Noise Certification Predictions for FJX-2-Powered Aircraft Using Analytic Methods
Thrust augmentation options for the Beta 2 two-stage-to-orbit vehicle
System Noise Prediction of the DGEN 380 Turbofan Engine
The design and performance estimates for the propulsion module for the booster of a TSTO vehicle