NASA NTRS · 20030062762
Turbine Aerodynamic Design System Improvements
Abstract
Presentation outline includes the following: 1. Volute manifold design and analysis methodology. 2. Meanline modification for compatibility with engine analysis code. Objective is to develop a manifold design methodology for turbines and pumps, and to enable rapid screening of candidate flow paths.
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Huber, Frank W., Griffin, Lisa W., Simpson, Steven P.. 2003-04-01. Turbine Aerodynamic Design System Improvements. https://ntrs.nasa.gov/citations/20030062762
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