41st AIAA Fluid Dynamics Conference and Exhibit 2011
DOI: 10.2514/6.2011-3720
|View full text |Cite
|
Sign up to set email alerts
|

Optimal Control of Unsteady Flows Using Discrete Adjoints

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
2
1

Citation Types

0
12
0

Year Published

2013
2013
2019
2019

Publication Types

Select...
3
3
3

Relationship

2
7

Authors

Journals

citations
Cited by 14 publications
(12 citation statements)
references
References 20 publications
0
12
0
Order By: Relevance
“…For a high-fidelity setup with millions of grid nodes explored in current work, this presents an impossible task for the reverse mode AD due to the memory overhead and can only be accomplished using advanced AD techniques such as reverse accumulation and checkpointing. 19 Future work will include performing optimizations that involve longer simulation times on the order of 10 4 time steps.…”
Section: Discussionmentioning
confidence: 99%
See 1 more Smart Citation
“…For a high-fidelity setup with millions of grid nodes explored in current work, this presents an impossible task for the reverse mode AD due to the memory overhead and can only be accomplished using advanced AD techniques such as reverse accumulation and checkpointing. 19 Future work will include performing optimizations that involve longer simulation times on the order of 10 4 time steps.…”
Section: Discussionmentioning
confidence: 99%
“…A good discussion of the two AD modes along with checkpointing techniques can be found in. 19 A quasi-Newton optimizer in which an estimate of the inverse Hessian based on the BFGS (Broyden-FletcherGoldfarb-Shanno) rank-two update formula is used to compute a search direction. 20 The step size is determined using a line search, which enforces the strong Wolfe conditions.…”
Section: Iic Optimization Frameworkmentioning
confidence: 99%
“…For a high-fidelity setup with millions of grid nodes explored in current work, this presents an impossible task for the reverse mode AD due to the memory overhead and can only be accomplished using advanced AD techniques such as reverse accumulation and checkpointing. 19 When the nearbody turbulence intensity measure is minimized, the design shows only marginal reduction in overall sound pressure level, even though the vorticity magnitude and the turbulence kinetic energy are both minimized in the wake region. However, when the objective function is changed to the root-mean-square of the pressure fluctuation at different off-body observation locations, the noise reduction is significant -12dB in the normal direction and up to 18dB in the upstream direction.…”
Section: Optimization Windowmentioning
confidence: 98%
“…Papadimitriou dpapadim@uth.gr In aerodynamics, the conventional adjoint approach to the optimisation of unsteady flows, based on the timeaccurate adjoint equations, has been applied to the drag minimisation of airfoils with deforming meshes (Mani and Mavriplis 2008;Mavriplis 2008), the optimisation of active unsteady flow control based on jets (Nielsen and Jones 2011;Nemili et al 2011), optimisation of rotors (Nielsen, Lee-Rausch, and Jones 2010), aeroelastic optimisation (Mani and Mavriplis 2009), flutter suppression (Palaniappan et al 2011;Zhang et al 2013), error estimation (Krakos and Darmofal 2010), uncertainty quantification (Wang 2008), etc.…”
Section: Introductionmentioning
confidence: 99%