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Title: An adjoint method for a high-order discretization of deforming domain conservation laws for optimization of flow problems

Journal Article · · Journal of Computational Physics

We report the fully discrete adjoint equations and the corresponding adjoint method are derived for a globally high-order accurate discretization of conservation laws on parametrized, deforming domains. The conservation law on the deforming domain is transformed into one on a fixed reference domain by the introduction of a time-dependent mapping that encapsulates the domain deformation and parametrization, resulting in an Arbitrary Lagrangian–Eulerian form of the governing equations. A high-order discontinuous Galerkin method is used to discretize the transformed equation in space and a high-order diagonally implicit Runge–Kutta scheme is used for the temporal discretization. Quantities of interest that take the form of space–time integrals are discretized in a solver-consistent manner. The corresponding fully discrete adjoint method is used to compute exact gradients of quantities of interest along the manifold of solutions of the fully discrete conservation law. These quantities of interest and their gradients are used in the context of gradient-based PDE-constrained optimization. The adjoint method is used to solve two optimal shape and control problems governed by the isentropic, compressible Navier–Stokes equations. The first optimization problem seeks the energetically optimal trajectory of a 2D airfoil given a required initial and final spatial position. The optimization solver, driven by gradients computed via the adjoint method, reduced the total energy required to complete the specified mission nearly an order of magnitude. The second optimization problem seeks the energetically optimal flapping motion and time-morphed geometry of a 2D airfoil given an equality constraint on the x-directed impulse generated on the airfoil. The optimization solver satisfied the impulse constraint to greater than 8 digits of accuracy and reduced the required energy between a factor of 2 and 10, depending on the value of the impulse constraint, as compared to the nominal configuration.

Research Organization:
Krell Institute, Ames, IA (United States); University of California, Berkeley, CA (United States)
Sponsoring Organization:
USDOE Office of Science (SC); USDOE National Nuclear Security Administration (NNSA)
Grant/Contract Number:
FG02-97ER25308; AC02-05CH11231
OSTI ID:
1533951
Alternate ID(s):
OSTI ID: 1359311
Journal Information:
Journal of Computational Physics, Vol. 326, Issue C; ISSN 0021-9991
Publisher:
ElsevierCopyright Statement
Country of Publication:
United States
Language:
English
Citation Metrics:
Cited by: 13 works
Citation information provided by
Web of Science

References (46)

Overview of Sensitivity Analysis and Shape Optimization for Complex Aerodynamic Configurations journal January 1999
Algorithm Developments for Discrete Adjoint Methods journal February 2003
Discrete Adjoint-Based Approach for Optimization Problems on Three-Dimensional Unstructured Meshes journal April 2007
ADjoint: An Approach for the Rapid Development of Discrete Adjoint Solvers journal April 2008
Massively parallel aerodynamic shape optimization journal January 1992
Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers journal May 1999
Optimal Control of Two- and Three-Dimensional Incompressible Navier–Stokes Flows journal September 1997
Flapping Wing Aerodynamics: Progress and Challenges journal September 2008
High-order CFD methods: current status and perspective: HIGH-ORDER CFD METHODS journal January 2013
Unsteady Discrete Adjoint Formulation for Two-Dimensional Flow Problems with Deforming Meshes journal June 2008
Discontinuous Galerkin solution of the Navier–Stokes equations on deformable domains journal April 2009
Optimum Shape Design for Unsteady Flows with Time-Accurate Continuous and Discrete Adjoint Method journal July 2007
Discrete Adjoint-Based Design Optimization of Unsteady Turbulent Flows on Dynamic Unstructured Grids journal June 2010
An Entropy Adjoint Approach to Mesh Refinement journal January 2010
Output error estimation strategies for discontinuous Galerkin discretizations of unsteady convection-dominated flows journal May 2011
Output-based mesh adaptation for high order Navier–Stokes simulations on deformable domains journal November 2013
Diagonally Implicit Runge–Kutta Methods for Stiff O.D.E.’s journal December 1977
Time dependent adjoint-based optimization for coupled fluid–structure problems journal July 2015
Self-Contained Automated Methodology for Optimal Flow Control journal May 1997
Unified Analysis of Discontinuous Galerkin Methods for Elliptic Problems journal January 2002
Adjoint Consistency Analysis of Discontinuous Galerkin Discretizations journal January 2007
Generalized adjoint consistent treatment of wall boundary conditions for compressible flows journal November 2015
hp -Adaptive Discontinuous Galerkin Finite Element Methods for First-Order Hyperbolic Problems journal January 2001
Three-dimensional shape optimization journal May 1982
A three-dimensional torsional spring analogy method for unstructured dynamic meshes journal February 2002
The Discrete Geometric Conservation Law and the Nonlinear Stability of ALE Schemes for the Solution of Flow Problems on Moving Grids journal December 2001
Runge-Kutta Discontinuous Galerkin Methods for Convection-Dominated Problems journal September 2001
Local-in-time adjoint-based method for design optimization of unsteady flows journal July 2010
Checkpointing Schemes for Adjoint Codes: Application to the Meteorological Model Meso-NH journal January 2001
An efficient exact adjoint of the parallel MIT General Circulation Model, generated via automatic differentiation journal October 2005
The Compact Discontinuous Galerkin (CDG) Method for Elliptic Problems journal January 2008
Progressive construction of a parametric reduced-order model for PDE-constrained optimization: PDE-CONSTRAINED OPTIMIZATION USING A PROGRESSIVELY CONSTRUCTED ROM journal December 2014
On the incompressible limit of the compressible navier-stokes equations journal January 1995
Incompressible Limit for Solutionsof the Isentropic Navier–Stokes Equationswith Dirichlet Boundary Conditions journal June 1999
Approximate Riemann solvers, parameter vectors, and difference schemes journal October 1981
Algorithm 778: L-BFGS-B: Fortran subroutines for large-scale bound-constrained optimization journal December 1997
A fully discrete adjoint method for optimization of flow problems on deforming domains with time-periodicity constraints journal November 2016
Unsteady aerodynamics and flow control for flapping wing flyers journal November 2003
Analytical Sensitivity Analysis of an Unsteady Vortex-Lattice Method for Flapping-Wing Optimization journal March 2010
Global optimization of actively morphing flapping wings journal August 2012
SNOPT: An SQP Algorithm for Large-Scale Constrained Optimization journal January 2002
Optimization of Flapping Airfoils For Maximum Thrust and Propulsive Efficiency journal November 2005
Simulation of Flow About Flapping Airfoils Using Finite Element Incompressible Flow Solver journal February 2001
Aerodynamic Multiobjective Design Exploration of a Flapping Airfoil Using a Navier-Stokes Solver
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