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      Analysis and Uncertainty Quantification of a Hybrid Laminar Flow Control System

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          Abstract

          This study aims to quantify suction velocities for hybrid laminar flow control of a vertical fin by taking data and model uncertainties into account. Because suction velocities cannot be measured directly, they are calculated using the Darcy–Forchheimer model, which needs the pressure distribution and porosity characteristics as input. Uncertainties in the pressure distribution are characterized using a novel data fusion method incorporating wind-tunnel and numerical data. Furthermore, geometrical uncertainties of the airfoil that alter the pressure distribution are considered. Two methods are proposed to model the porosity characteristics of the surface: one of which uses a local representation, and the other a global representation. In addition, the modeling error of the Darcy–Forchheimer model is estimated. These input uncertainties are quantified and propagated by Monte Carlo sampling through the Darcy–Forchheimer model. It reveals that local information on the porosity characteristics is essential for accurate suction velocity estimates for this specific application. A sensitivity study shows that the most influential contribution to the variance of suction velocities is the uncertainty in the porosity characteristics, followed by uncertainties in the pressure distribution. The model error and uncertainties in the reference pressure are shown to have a negligible influence.

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            Bayesian calibration of computer models

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              The Proper Orthogonal Decomposition in the Analysis of Turbulent Flows

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                Author and article information

                Contributors
                Conference
                aiaaj
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics
                1533-385X
                29 July 2022
                October 2022
                : 60
                : 10
                : 5735-5749
                Affiliations
                Technische Universität Braunschweig , D-38108 Brunswick, Germany
                Technische Universität Braunschweig , D-38106 Brunswick, Germany
                DLR, German Aerospace Center , D-38108 Brunswick, Germany
                Technische Universität Braunschweig , D-38108 Brunswick, Germany
                Author notes
                [*]

                Research Assistant, Institute of Fluid Mechanics, Hermann-Blenk-Str. 37.

                [†]

                Junior Professor, Institut für Dynamik und Schwingungen, Schleinitzstr. 20.

                [‡]

                Research Scientist, Institute of Aerodynamics and Flow Technology, Center for Computer Applications in AeroSpace Science and Engineering Department, Lilienthalplatz 7.

                [§]

                Team Leader, Institute of Aerodynamics and Flow Technology, Center for Computer Applications in AeroSpace Science and Engineering Department, Lilienthalplatz 7.

                [¶]

                Research Assistant, Institute of Aerodynamics and Flow Technology, Lilienthalplatz 7.

                [**]

                Head of the Institute, Institute of Fluid Mechanics, Hermann-Blenk-Str. 37.

                [††]

                Research Group Leader, Institute of Fluid Mechanics, Hermann-Blenk-Str. 37.

                Author information
                https://orcid.org/0000-0002-1277-7509
                Article
                J061745 J061745
                10.2514/1.J061745
                a08143d6-7fd9-4fe4-99cf-7e89c225f989
                Copyright © 2022 by A. Barklage, U. Römer, A. Bertram, P. Bekemeyer, J. Himisch, R. Radespiel, and C. Badyra. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 17 February 2022
                : 15 May 2022
                : 17 June 2022
                Page count
                Figures: 14, Tables: 2
                Funding
                Funded by: Clean Sky 2
                Award ID: 882646
                Categories
                Regular Articles
                p2263, Fluid Dynamics
                p1804, Aerodynamics
                p2030, Wind Tunnels
                p3282, Computational Fluid Dynamics
                p1976, Flow Regimes
                p1975, Boundary Layers
                p6221, Slip (Aerodynamics)
                p3997, Monte Carlo Method
                p20543, Aerodynamic Performance
                p3304, Numerical Analysis

                Engineering,Physics,Mechanical engineering,Space Physics
                German Dutch Wind Tunnels,Hybrid Laminar Flow Control,Data Fusion,Airfoil,Reynolds Averaged Navier Stokes,Cumulative Distribution Function,Courant Friedrichs Lewy,Natural Laminar Flow,Laminar to Turbulent Transition,Radial Basis Function Kernel

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