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Opportunities for Breakthroughs in Large-Scale Computational Simulation and DesignOpportunities for breakthroughs in the large-scale computational simulation and design of aerospace vehicles are presented. Computational fluid dynamics tools to be used within multidisciplinary analysis and design methods are emphasized. The opportunities stem from speedups and robustness improvements in the underlying unit operations associated with simulation (geometry modeling, grid generation, physical modeling, analysis, etc.). Further, an improved programming environment can synergistically integrate these unit operations to leverage the gains. The speedups result from reducing the problem setup time through geometry modeling and grid generation operations, and reducing the solution time through the operation counts associated with solving the discretized equations to a sufficient accuracy. The opportunities are addressed only at a general level here, but an extensive list of references containing further details is included. The opportunities discussed are being addressed through the Fast Adaptive Aerospace Tools (FAAST) element of the Advanced Systems Concept to Test (ASCoT) and the third Generation Reusable Launch Vehicles (RLV) projects at NASA Langley Research Center. The overall goal is to enable greater inroads into the design process with large-scale simulations.
Document ID
20020060131
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Alexandrov, Natalia
(NASA Langley Research Center Hampton, VA United States)
Alter, Stephen J.
(NASA Langley Research Center Hampton, VA United States)
Atkins, Harold L.
(NASA Langley Research Center Hampton, VA United States)
Bey, Kim S.
(NASA Langley Research Center Hampton, VA United States)
Bibb, Karen L.
(NASA Langley Research Center Hampton, VA United States)
Biedron, Robert T.
(NASA Langley Research Center Hampton, VA United States)
Carpenter, Mark H.
(NASA Langley Research Center Hampton, VA United States)
Cheatwood, F. McNeil
(NASA Langley Research Center Hampton, VA United States)
Drummond, Philip J.
(NASA Langley Research Center Hampton, VA United States)
Gnoffo, Peter A.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2002
Subject Category
Aerodynamics
Report/Patent Number
L-18196
NASA/TM-2002-211747
NAS 1.15:211747
Report Number: L-18196
Report Number: NASA/TM-2002-211747
Report Number: NAS 1.15:211747
Funding Number(s)
PROJECT: RTOP 706-31-21-80
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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