Turbo Design(LEW-20578-1)

aeronautics
Turbo Design
(LEW-20578-1)
Overview
Turbo Design (TD) is a radial equilibrium turbomachinery design tool for computing the blade angles for a given design condition that matches the massflow. This tool can also be used to calculate the performance if blade angles are already known. Turbo Design has been written from scratch solving the governing equations. It is meant to be an education and research tool for incorporating machine learning loss models in turbomachinery design.
Software Details

Category
Aeronautics
Reference Number
LEW-20578-1
Release Type
Open Source
Operating System
Windows, Linux, OS X
Contact Us About This Technology

Glenn Research Center
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