Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Open Access Guideline
Open Access Guideline
Postgraduate Thesis Guideline
Postgraduate Thesis Guideline
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
Overview of activities in stochastic data assimilation for applications in aerodynamics
Date
2012-10-03
Author
Dwight, R P
De Baar, J H S
Sciacchitano, A
Perçin, Mustafa
Bijl, Hester
Scarano, Fulvio
Metadata
Show full item record
Item Usage Stats
137
views
0
downloads
Cite This
In this conspectus paper we present a brief summary of a variety of recent activities in data assimilation performed at the Aerodynamics Section of the TU Delft. We hope to demonstrate a few of the exciting possibilities for combining experimental data and numerical models, improving the capability of both. Our activities are bound by a common theme of combining experimental wind-tunnel measurements and CFD simulations in order to (i) improve fidelity of experimental data, (ii) obtain estimates of unmeasured quantities, (iii) estimate modeling error and parametric uncertainty in simulation. The methodologies we use depends strongly on the application, but all have Bayesian inference at their root with some statistical model representing the relation between measurement and simulation. Bayesian statistics offers a coherent and flexible framework for describing solutions of the ill-posed problems that arise in this analysis of data, but new numerical methods are needed to find these solutions efficiently.
Subject Keywords
Bayesian inference,
,
Uncertainty quantification,
,
Data assimilation,
,
Aerodynamics,
,
CFD,
,
Uncertainty quantification,
,
Model inadequacy,
,
Kriging.
URI
https://hdl.handle.net/11511/88126
Collections
Department of Aerospace Engineering, Conference / Seminar
Suggestions
OpenMETU
Core
LOOSE COUPLING OF SU2 MULTIPHYSICS CODE WITH PATO TO ANALYZE THE SURFACE RECESSION EFFECT ON SURFACE HEAT FLUX
Çelik, Mutlu; Uğur, Ömür; Eyi, Sinan; Department of Scientific Computing (2022-12-30)
In this thesis, open source softwares SU2 Multiphysics and The Porous material Analysis Toolbox (PATO) based on OpenFOAM are used to conduct loosely coupled analysis of hypersonic non-equilibrium flow and thermochemical ablation. Both solvers have become prominent open source softwares with numerous validation and verification cases. NEMO, the non-equilibrium modeling solver of SU2 is used to model chemically reactive and non-equilibrium flows by integrating thermochemistry library of Mutation++. SU2-NEMO s...
Environmental aesthetics of the rural architectural tradition in the Mediterranean highlander settlement: the case study of Ürünlü
Kavas, Kemal Reha; Erzen, Jale Adile; Department of History of Architecture (2009)
This thesis formulates a conceptual framework to account for the rural architectural traditions. The proposal is presented by referring to Ürünlü, a Mediterranean highland settlement in Southwestern Turkey. The thesis' basic assumption is the environmental coherence of the traditional rural culture. Environmental aesthetics provides the conceptual basis through which architectural elements of the environmental coherence are investigated. Environmental aesthetics enhances the inclusive conceptions of "enviro...
Spatial control of a smart beam
Kircali, Omer Faruk; Yaman, Yavuz; Nalbantoglu, Volkan; Şahin, Melin; Karadal, Fatih Mutlu; Ulker, Fatma Demet (2008-08-01)
This study presents the design and implementation of a spatial H(infinity) controller for the active vibration control of a smart beam. The smart beam was modeled by assumed-modes method that results in a model including large number of resonant modes. The order of the model was reduced by direct model truncation and the model correction technique was applied to compensate the effect of the contribution of the out of range modes to the dynamics of the system. Additionally, spatial identification of the beam...
Atmospheric boundary layer simulation in a short wind tunnel
Shojaee, S. M. N.; Uzol, Oğuz; Kurç, Özgür (2014-02-01)
This paper presents the design, computational analysis and experimental study of passive device configurations which utilized in the Ankara Wind Tunnel to simulate the atmospheric boundary layer within the test section. The study here is part of a joint project between the Aerospace and Civil Engineering Departments at Middle East Technical University, which involves testing of high-rise building models in the Ankara Wind Tunnel. The design consists of spires and rows of cubical surface roughness elements a...
Verification of Modular Diagnosability With Local Specifications for Discrete-Event Systems
Schmidt, Klaus Verner (Institute of Electrical and Electronics Engineers (IEEE), 2013-09-01)
In this paper, we study the diagnosability verification for modular discrete-event systems (DESs), i.e., DESs that are composed of multiple components. We focus on a particular modular architecture, where each fault in the system must be uniquely identified by the modular component where it occurs and solely based on event observations of that component. Hence, all diagnostic computations for faults to be detected in this architecture can be performed locally on the respective modular component, and the obt...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
R. P. Dwight, J. H. S. De Baar, A. Sciacchitano, M. Perçin, H. Bijl, and F. Scarano, “Overview of activities in stochastic data assimilation for applications in aerodynamics,” Tokyo, Japonya, 2012, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/88126.