An efficient non-intrusive reduced basis model for high dimensional stochastic problems in CFD. (15th October 2016)
- Record Type:
- Journal Article
- Title:
- An efficient non-intrusive reduced basis model for high dimensional stochastic problems in CFD. (15th October 2016)
- Main Title:
- An efficient non-intrusive reduced basis model for high dimensional stochastic problems in CFD
- Authors:
- Kumar, Dinesh
Raisee, Mehrdad
Lacor, Chris - Abstract:
- Highlights: An efficient reduced basis model for stochastic applications is proposed. The model is implemented in the framework of non-intrusive polynomial chaos. The model is applied to two high-dimensional stochastic CFD problems. The CPU cost of the proposed model is 5–10 times lower than the classical model. Abstract: The major challenge industrial applications of uncertainty quantification (UQ) are facing, is the curse of dimensionality as a result of a large number of uncertainties. In this work, an efficient non-intrusive model reduction scheme is presented for UQ using proper orthogonal decomposition and a non-intrusive polynomial chaos approach based on regression. The main idea is to extract the optimal orthogonal basis via inexpensive calculations on a coarse mesh and then use this basis for the fine scale analysis. To validate the developed non-intrusive, reduced-order model, it is applied to two CFD type applications: (1) flow over a 2D RAE2822 airfoil and (2) the NASA Rotor 37, a transonic axial flow compressor. For the RAE2822, the surface of the airfoil is assumed to be stochastic and is defined as a random field with a given covariance and modeled using Karhunen–Lo e ` ve expansion. For the NASA Rotor 37, the geometry of the rotor blade is parameterized into 2D sections of airfoils. A total of 21 uncertain parameters is considered containing both operational and geometrical uncertainties. The statistical results are compared with those of the standardHighlights: An efficient reduced basis model for stochastic applications is proposed. The model is implemented in the framework of non-intrusive polynomial chaos. The model is applied to two high-dimensional stochastic CFD problems. The CPU cost of the proposed model is 5–10 times lower than the classical model. Abstract: The major challenge industrial applications of uncertainty quantification (UQ) are facing, is the curse of dimensionality as a result of a large number of uncertainties. In this work, an efficient non-intrusive model reduction scheme is presented for UQ using proper orthogonal decomposition and a non-intrusive polynomial chaos approach based on regression. The main idea is to extract the optimal orthogonal basis via inexpensive calculations on a coarse mesh and then use this basis for the fine scale analysis. To validate the developed non-intrusive, reduced-order model, it is applied to two CFD type applications: (1) flow over a 2D RAE2822 airfoil and (2) the NASA Rotor 37, a transonic axial flow compressor. For the RAE2822, the surface of the airfoil is assumed to be stochastic and is defined as a random field with a given covariance and modeled using Karhunen–Lo e ` ve expansion. For the NASA Rotor 37, the geometry of the rotor blade is parameterized into 2D sections of airfoils. A total of 21 uncertain parameters is considered containing both operational and geometrical uncertainties. The statistical results are compared with those of the standard polynomial chaos method. The results show that the developed model produces statistical results with good accuracy. It is found that the memory requirements and the computational cost of the reduced-order model is 5–10 times lower than that of the standard polynomial chaos. … (more)
- Is Part Of:
- Computers & fluids. Volume 138(2016)
- Journal:
- Computers & fluids
- Issue:
- Volume 138(2016)
- Issue Display:
- Volume 138, Issue 2016 (2016)
- Year:
- 2016
- Volume:
- 138
- Issue:
- 2016
- Issue Sort Value:
- 2016-0138-2016-0000
- Page Start:
- 67
- Page End:
- 82
- Publication Date:
- 2016-10-15
- Subjects:
- Stochastic -- Polynomial Chaos -- Proper Orthogonal Decomposition -- Reduced basis -- Model Reduction
Fluid dynamics -- Data processing -- Periodicals
532.050285 - Journal URLs:
- http://www.journals.elsevier.com/computers-and-fluids/ ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.compfluid.2016.08.015 ↗
- Languages:
- English
- ISSNs:
- 0045-7930
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 3394.690000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 1439.xml