NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
National Combustion Code Parallel Performance EnhancementsThe National Combustion Code (NCC) is being developed by an industry-government team for the design and analysis of combustion systems. The unstructured grid, reacting flow code uses a distributed memory, message passing model for its parallel implementation. The focus of the present effort has been to improve the performance of the NCC code to meet combustor designer requirements for model accuracy and analysis turnaround time. Improving the performance of this code contributes significantly to the overall reduction in time and cost of the combustor design cycle. This report describes recent parallel processing modifications to NCC that have improved the parallel scalability of the code, enabling a two hour turnaround for a 1.3 million element fully reacting combustion simulation on an SGI Origin 2000.
Document ID
20020085102
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Quealy, Angela
(QSS Group, Inc. Cleveland, OH United States)
Benyo, Theresa
Date Acquired
September 7, 2013
Publication Date
August 1, 2002
Subject Category
Computer Programming And Software
Report/Patent Number
NAS 1.26:211340
E-13151
AIAA Paper 2002-3706
NASA/CR-2002-211340
Report Number: NAS 1.26:211340
Report Number: E-13151
Report Number: AIAA Paper 2002-3706
Report Number: NASA/CR-2002-211340
Meeting Information
Meeting: 38th Joint Propulsion Conference and Exhibit
Location: Indianapolis, IN
Country: United States
Start Date: July 7, 2002
End Date: July 10, 2002
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, American Society for Electrical Engineers, Society of Automotive Engineers, Inc.
Funding Number(s)
PROJECT: RTOP 704-20-13
CONTRACT_GRANT: NAS3-00145
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available