CSPAN Axial-Flow Compressor Conceptual Design Code(LEW-16074-1)

propulsion
CSPAN Axial-Flow Compressor Conceptual Design Code
(LEW-16074-1)
Overview
This span-line analysis technology uses isentropic simple radial equilibrium to determine a flow path.
This software is only available for use by federal employees and contractors to the federal government working on projects where this tool would be applicable.

Software Details

Category
Propulsion
Reference Number
LEW-16074-1
Release Type
U.S. Government Purpose Release
Operating System
Contact Us About This Technology

Glenn Research Center
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