Continuum Sensitivity Method for Nonlinear Dynamic Aeroelasticity

In this dissertation, a continuum sensitivity method is developed for efficient and accurate computation of design derivatives for nonlinear aeroelastic structures subject to transient<br />aerodynamic loads. The continuum sensitivity equations (CSE) are a set of linear partial<br />diff...

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Main Author: Liu, Shaobin
Other Authors: Aerospace and Ocean Engineering
Format: Others
Published: Virginia Tech 2013
Subjects:
Online Access:http://hdl.handle.net/10919/23282
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spelling ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-232822021-11-04T05:33:59Z Continuum Sensitivity Method for Nonlinear Dynamic Aeroelasticity Liu, Shaobin Aerospace and Ocean Engineering Canfield, Robert A. Hajj, Muhammad R. Kapania, Rakesh K. Roy, Christopher J. Patil, Mayuresh J. Continuum Sensitivity Shape Sensitivity Aeroelasticity Optimization Fluid-structure interaction In this dissertation, a continuum sensitivity method is developed for efficient and accurate computation of design derivatives for nonlinear aeroelastic structures subject to transient<br />aerodynamic loads. The continuum sensitivity equations (CSE) are a set of linear partial<br />differential equations (PDEs) obtained by differentiating the original governing equations of<br />the physical system. The linear CSEs may be solved by using the same numerical method<br />used for the original analysis problem. The material (total) derivative, the local (partial)<br />derivative, and their relationship is introduced for shape sensitivity analysis. The CSEs are<br />often posed in terms of local derivatives (local form) for fluid applications and in terms of total<br />derivatives (total form) for structural applications. The local form CSE avoids computing<br />mesh sensitivity throughout the domain, as required by discrete analytic sensitivity methods.<br />The application of local form CSEs to built-up structures is investigated. The difficulty<br />of implementing local form CSEs for built-up structures due to the discontinuity of local<br />sensitivity variables is pointed out and a special treatment is introduced. The application<br />of the local form and the total form CSE methods to aeroelastic problems are compared.<br />Their advantages and disadvantages are discussed, based on their derivations, efficiency,<br />and accuracy. Under certain conditions, the total form continuum method is shown to be<br />equivalent to the analytic discrete method, after discretization, for systems governed by a<br />general second-order PDE. The advantage of the continuum sensitivity method is that less<br />information of the source code of the analysis solver is required. Verification examples are<br />solved for shape sensitivity of elastic, fluid and aeroelastic problems. Ph. D. 2013-06-29T08:00:17Z 2013-06-29T08:00:17Z 2013-06-28 Dissertation vt_gsexam:1344 http://hdl.handle.net/10919/23282 In Copyright http://rightsstatements.org/vocab/InC/1.0/ ETD application/pdf Virginia Tech
collection NDLTD
format Others
sources NDLTD
topic Continuum Sensitivity
Shape Sensitivity
Aeroelasticity
Optimization
Fluid-structure interaction
spellingShingle Continuum Sensitivity
Shape Sensitivity
Aeroelasticity
Optimization
Fluid-structure interaction
Liu, Shaobin
Continuum Sensitivity Method for Nonlinear Dynamic Aeroelasticity
description In this dissertation, a continuum sensitivity method is developed for efficient and accurate computation of design derivatives for nonlinear aeroelastic structures subject to transient<br />aerodynamic loads. The continuum sensitivity equations (CSE) are a set of linear partial<br />differential equations (PDEs) obtained by differentiating the original governing equations of<br />the physical system. The linear CSEs may be solved by using the same numerical method<br />used for the original analysis problem. The material (total) derivative, the local (partial)<br />derivative, and their relationship is introduced for shape sensitivity analysis. The CSEs are<br />often posed in terms of local derivatives (local form) for fluid applications and in terms of total<br />derivatives (total form) for structural applications. The local form CSE avoids computing<br />mesh sensitivity throughout the domain, as required by discrete analytic sensitivity methods.<br />The application of local form CSEs to built-up structures is investigated. The difficulty<br />of implementing local form CSEs for built-up structures due to the discontinuity of local<br />sensitivity variables is pointed out and a special treatment is introduced. The application<br />of the local form and the total form CSE methods to aeroelastic problems are compared.<br />Their advantages and disadvantages are discussed, based on their derivations, efficiency,<br />and accuracy. Under certain conditions, the total form continuum method is shown to be<br />equivalent to the analytic discrete method, after discretization, for systems governed by a<br />general second-order PDE. The advantage of the continuum sensitivity method is that less<br />information of the source code of the analysis solver is required. Verification examples are<br />solved for shape sensitivity of elastic, fluid and aeroelastic problems. === Ph. D.
author2 Aerospace and Ocean Engineering
author_facet Aerospace and Ocean Engineering
Liu, Shaobin
author Liu, Shaobin
author_sort Liu, Shaobin
title Continuum Sensitivity Method for Nonlinear Dynamic Aeroelasticity
title_short Continuum Sensitivity Method for Nonlinear Dynamic Aeroelasticity
title_full Continuum Sensitivity Method for Nonlinear Dynamic Aeroelasticity
title_fullStr Continuum Sensitivity Method for Nonlinear Dynamic Aeroelasticity
title_full_unstemmed Continuum Sensitivity Method for Nonlinear Dynamic Aeroelasticity
title_sort continuum sensitivity method for nonlinear dynamic aeroelasticity
publisher Virginia Tech
publishDate 2013
url http://hdl.handle.net/10919/23282
work_keys_str_mv AT liushaobin continuumsensitivitymethodfornonlineardynamicaeroelasticity
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