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MSFC Turbine Performance Optimization (TPO) Technology Verification 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, validated aerodynamic design, analysis, and optimization system is required.
Document ID
20020050507
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Griffin, Lisa W. (NASA Marshall Space Flight Center Huntsville, AL United States)
Dorney, Daniel J. (NASA Marshall Space Flight Center Huntsville, AL United States)
Snellgrove, Lauren M. (NASA Marshall Space Flight Center Huntsville, AL United States)
Zoladz, Thomas F. (NASA Marshall Space Flight Center Huntsville, AL United States)
Stroud, Richard T. (NASA Marshall Space Flight Center Huntsville, AL United States)
Turner, James E.
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Mechanical Engineering
Meeting Information
Meeting: JANNAF 26th Airbreathing Propulsion Subcommittee Meeting
Location: Destin, FL
Country: United States
Start Date: April 8, 2002
End Date: April 12, 2002
Sponsors: Department of the Army, Department of the Navy, NASA Headquarters, Department of the Air Force
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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