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Distributed Turboelectric Propulsion Distributed Turboelectric Propulsion for Hybrid Wing Body Aircraft
GE90 Diagram Ultrahigh Bypass Ratio Propulsion Systems Studied
P-BEAT Process-based cost code P-BEAT: A Process-Based Economic Analysis Tool
Analysis Linking An Environmental Design Space to Assess Aircraft Technology and Operational Trades
Adaptive Flow Control Technologies Adaptive Engine Technologies for Aviation CO2 Emissions Reduction
Aviation Safety and Security Logo Risk Assessment and Technology Portfolio Prioritization Using Logic-Evolved Decision Analysis Methodologies for Aviation Security
Aircraft Noise Emissions Analytical Core Noise Model Improved for Modern Turbofan Engines
PW4000 Diagram Water Injection in Commercial Aircraft Investigated for Increasing Engine Life and Reducing Costs and Emissions
Tiny Engines, Big Rewards Tiny Engines, Big Rewards:
A Cruise-Efficient, Short Takeoff & Landing Vehicle is Analyzed
42nd Joint Propulsion Conference PSA Branch's Participation in the 42nd Joint Propulsion Conference
Electric Airplane Performance of a Fuel-Cell-Powered, Small Electric Airplane Assessed
GE90 Diagram Computer Code for Gas Turbine Engine Weight and Disk Life Estimation Improved
Software of the Year Award NPSS Team Wins Prestigious NASA Software of the Year Award
High-Wing Concept Airplane Advanced Engine Cycles Analyzed for Turbofans With Variable-Area Fan Nozzles Actuated by a Shape Memory Alloy
Overwing Propulsion Coinfiguration Noise Reduction Benefits Analyzed for Over-the-Wing-Mounted Advanced Turbofan Engines
High Speed Civil Transport Minimum Climb to Cruise Noise Trajectories Modeled for the High Speed Civil Transport


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Last Updated: November 4, 2016