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Toward Automatic Verification of Goal-Oriented Flow SimulationsWe demonstrate the power of adaptive mesh refinement with adjoint-based error estimates in verification of simulations governed by the steady Euler equations. The flow equations are discretized using a finite volume scheme on a Cartesian mesh with cut cells at the wall boundaries. The discretization error in selected simulation outputs is estimated using the method of adjoint-weighted residuals. Practical aspects of the implementation are emphasized, particularly in the formulation of the refinement criterion and the mesh adaptation strategy. Following a thorough code verification example, we demonstrate simulation verification of two- and three-dimensional problems. These involve an airfoil performance database, a pressure signature of a body in supersonic flow and a launch abort with strong jet interactions. The results show reliable estimates and automatic control of discretization error in all simulations at an affordable computational cost. Moreover, the approach remains effective even when theoretical assumptions, e.g., steady-state and solution smoothness, are relaxed.
Document ID
20150000864
Acquisition Source
Ames Research Center
Document Type
Technical Memorandum (TM)
Authors
Nemec, Marian
(Science and Technology Corp. Moffett Field, CA, United States)
Aftosmis, Michael J.
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
January 30, 2015
Publication Date
August 1, 2014
Subject Category
Numerical Analysis
Aerodynamics
Report/Patent Number
ARC-E-DAA-TN17393
NASA/TM-2014-218386
Report Number: ARC-E-DAA-TN17393
Report Number: NASA/TM-2014-218386
Funding Number(s)
CONTRACT_GRANT: NNA10DF26C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Simulations
Verification
Automatic
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