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CFD Vision 2030 Study: A Path to Revolutionary Computational AerosciencesThis report documents the results of a study to address the long range, strategic planning required by NASA's Revolutionary Computational Aerosciences (RCA) program in the area of computational fluid dynamics (CFD), including future software and hardware requirements for High Performance Computing (HPC). Specifically, the "Vision 2030" CFD study is to provide a knowledge-based forecast of the future computational capabilities required for turbulent, transitional, and reacting flow simulations across a broad Mach number regime, and to lay the foundation for the development of a future framework and/or environment where physics-based, accurate predictions of complex turbulent flows, including flow separation, can be accomplished routinely and efficiently in cooperation with other physics-based simulations to enable multi-physics analysis and design. Specific technical requirements from the aerospace industrial and scientific communities were obtained to determine critical capability gaps, anticipated technical challenges, and impediments to achieving the target CFD capability in 2030. A preliminary development plan and roadmap were created to help focus investments in technology development to help achieve the CFD vision in 2030.
Document ID
20140003093
Document Type
Contractor Report (CR)
Authors
Jeffrey P Slotnick (Boeing (United States) Chicago, Illinois, United States)
Abdollah Khodadoust (Boeing (United States) Chicago, Illinois, United States)
Juan Alonso (Stanford University Stanford, California, United States)
David Darmofal (Massachusetts Institute of Technology Cambridge, Massachusetts, United States)
William Gropp (National Center for Supercomputing Applications Urbana, Illinois, United States)
Elizabeth Lurie (Pratt & Whitney United Technologies Corp. East Hartford, CT, United States)
Dimitri J Mavriplis (University of Wyoming Laramie, Wyoming, United States)
Date Acquired
April 16, 2014
Publication Date
March 1, 2014
Subject Category
Aeronautics (General)
Report/Patent Number
NF1676L-18332
NASA/CR-2014-218178
Funding Number(s)
CONTRACT_GRANT: NNL08AA16B
TASK: NNL12AD05T
WBS: WBS 794072.02.07.02.03
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.

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