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Turbine Performance Optimization Task StatusCapability to optimize for turbine performance and accurately predict unsteady loads will allow for increased reliability, Isp, and thrust-to-weight. The development of a fast, accurate aerodynamic design, analysis, and optimization system is required.
Document ID
20010037813
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Griffin, Lisa W. (NASA Marshall Space Flight Center Huntsville, AL United States)
Turner, James E.
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: Fluids Workshop
Location: Huntsville, AL
Country: United States
Start Date: April 4, 2001
End Date: April 5, 2001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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