Research & Technology 1997
Photo of Gas Turbine Engine Simulation

High Speed Systems
High Speed Research--Propulsion Project Accomplishments

Propulsion Systems Analysis
Minimum Climb to Cruise Noise Trajectories for the High Speed Civil Transport
Inlet Performance Analysis Code Developed
Conceptual Design Method Developed for Advanced Propulsion Nozzles

Computing and Interdisciplinary Systems
Multiphysics Code Demonstrated for Propulsion Applications
Flow of a Gas Turbine Engine Low-Pressure Subsystem Simulated


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Last updated April 14, 1998, by Nancy.L.Obryan@nasa.gov


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