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Flugtriebwerk
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Hot Corrosion Damage Modeling in Aeroengines Based on Performance and Flight Mission
Using Working Parameters to Control Formation and Shape of Lotus-Type Pores
Computational Analysis of a Wing Designed for the X-57 Distributed Electric Propulsion Aircraft
Design and Development of a 200-kW Turbo-Electric Distributed Propulsion Testbed
Modeling Scramjet Flows with Variable Turbulent Prandtl and Schmidt Numbers
Propulsion Simulations Using Advanced Turbulence Models with the Unstructured Grid CFD Tool, TetrUSS
Uncontained Engine Debris Analysis Using the Uncontained Engine Debris Damage Assessment Model
The Computing And Interdisciplinary Systems Office: Annual Review and Planning Meeting
Advanced Methods for Aircraft Engine Thrust and Noise Benefits: Nozzle-Inlet Flow Analysis
The NPARC Alliance Verification and Validation Archive
Advanced Models for Aeroelastic Analysis of Propulsion Systems
P-51 Mustang As an Escort Fighter: Development Beyond Drop Tanks to an Independent Air Force