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CFD in the context of IHPTET: The Integrated High Performance Turbine Technology ProgramThe Integrated High Performance Turbine Engine Technology (IHPTET) Program is an integrated DOD/NASA technology program designed to double the performance capability of today's most advanced military turbine engines as we enter the twenty-first century. Computational Fluid Dynamics (CFD) is expected to play an important role in the design/analysis of specific configurations within this complex machine. In order to do this, a plan is being developed to ensure the timely impact of CFD on IHPTET. The developing philosphy of CFD in the context of IHPTET is discussed. The key elements in the developing plan and specific examples of state-of-the-art CFD efforts which are IHPTET turbine engine relevant are discussed.
Document ID
19890016803
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Simoneau, Robert J.
(NASA Lewis Research Center Cleveland, OH, United States)
Hudson, Dale A.
(Air Force Wright Research and Development Center Wright-Patterson AFB, OH., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 89-2904
NASA-TM-102132
E-4868
NAS 1.15:102132
Report Number: AIAA PAPER 89-2904
Report Number: NASA-TM-102132
Report Number: E-4868
Report Number: NAS 1.15:102132
Meeting Information
Meeting: Joint Propulsion Conference
Location: Monterey, CA
Country: United States
Start Date: July 10, 1989
End Date: July 12, 1989
Sponsors: ASME, SAE, ASEE, AIAA
Accession Number
89N26174
Funding Number(s)
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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