Thermal Characterization of Complex Aerospace Structures

Predicting the performance of complex structures exposed to harsh thermal environments is a crucial issue in many of today's aerospace and space designs. To predict the thermal stresses a structure might be exposed to, the thermal properties of the independent materials used in the design of t...

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Main Author: Hanuska, Alexander Robert Jr.
Other Authors: Mechanical Engineering
Format: Others
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/36617
http://scholar.lib.vt.edu/theses/available/etd-32298-85910/
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spelling ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-366172020-09-29T05:47:10Z Thermal Characterization of Complex Aerospace Structures Hanuska, Alexander Robert Jr. Mechanical Engineering Scott, Elaine P. Vick, Brian L. Diller, Thomas E. Parameter Estimation Aerospace Structures Genetic Algorithm Predicting the performance of complex structures exposed to harsh thermal environments is a crucial issue in many of today's aerospace and space designs. To predict the thermal stresses a structure might be exposed to, the thermal properties of the independent materials used in the design of the structure need to be known. Therefore, a noninvasive estimation procedure involving Genetic Algorithms was developed to determine the various thermal properties needed to adequately model the Outer Wing Subcomponent (OWS), a structure located at the trailing edge of the High Speed Civil Transport's (HSCT) wing tip. Due to the nature of the nonlinear least-squares estimation method used in this study, both theoretical and experimental temperature histories were required. Several one-dimensional and two-dimensional finite element models of the OWS were developed to compute the transient theoretical temperature histories. The experimental data were obtained from optimized experiments that were run at various surrounding temperature settings to investigate the temperature dependence of the estimated properties. An experimental optimization was performed to provide the most accurate estimates and reduce the confidence intervals. The simultaneous estimation of eight thermal properties, including the volumetric heat capacities and out-of-plane thermal conductivities of the facesheets, the honeycomb, the skins, and the torque tubes, was successfully completed with the one-dimensional model and the results used to evaluate the remaining in-plane thermal conductivities of the facesheets, the honeycomb, the skins, and the torque tubes with the two-dimensional model. Although experimental optimization did not eliminate all correlation between the parameters, the minimization procedure based on the Genetic Algorithm performed extremely well, despite the high degree of correlation and low sensitivity of many of the parameters. Master of Science 2014-03-14T20:51:17Z 2014-03-14T20:51:17Z 1998-04-16 1998-04-16 1999-04-24 1998-04-24 Thesis etd-32298-85910 http://hdl.handle.net/10919/36617 http://scholar.lib.vt.edu/theses/available/etd-32298-85910/ thesis.pdf In Copyright http://rightsstatements.org/vocab/InC/1.0/ application/pdf Virginia Tech
collection NDLTD
format Others
sources NDLTD
topic Parameter Estimation
Aerospace Structures
Genetic Algorithm
spellingShingle Parameter Estimation
Aerospace Structures
Genetic Algorithm
Hanuska, Alexander Robert Jr.
Thermal Characterization of Complex Aerospace Structures
description Predicting the performance of complex structures exposed to harsh thermal environments is a crucial issue in many of today's aerospace and space designs. To predict the thermal stresses a structure might be exposed to, the thermal properties of the independent materials used in the design of the structure need to be known. Therefore, a noninvasive estimation procedure involving Genetic Algorithms was developed to determine the various thermal properties needed to adequately model the Outer Wing Subcomponent (OWS), a structure located at the trailing edge of the High Speed Civil Transport's (HSCT) wing tip. Due to the nature of the nonlinear least-squares estimation method used in this study, both theoretical and experimental temperature histories were required. Several one-dimensional and two-dimensional finite element models of the OWS were developed to compute the transient theoretical temperature histories. The experimental data were obtained from optimized experiments that were run at various surrounding temperature settings to investigate the temperature dependence of the estimated properties. An experimental optimization was performed to provide the most accurate estimates and reduce the confidence intervals. The simultaneous estimation of eight thermal properties, including the volumetric heat capacities and out-of-plane thermal conductivities of the facesheets, the honeycomb, the skins, and the torque tubes, was successfully completed with the one-dimensional model and the results used to evaluate the remaining in-plane thermal conductivities of the facesheets, the honeycomb, the skins, and the torque tubes with the two-dimensional model. Although experimental optimization did not eliminate all correlation between the parameters, the minimization procedure based on the Genetic Algorithm performed extremely well, despite the high degree of correlation and low sensitivity of many of the parameters. === Master of Science
author2 Mechanical Engineering
author_facet Mechanical Engineering
Hanuska, Alexander Robert Jr.
author Hanuska, Alexander Robert Jr.
author_sort Hanuska, Alexander Robert Jr.
title Thermal Characterization of Complex Aerospace Structures
title_short Thermal Characterization of Complex Aerospace Structures
title_full Thermal Characterization of Complex Aerospace Structures
title_fullStr Thermal Characterization of Complex Aerospace Structures
title_full_unstemmed Thermal Characterization of Complex Aerospace Structures
title_sort thermal characterization of complex aerospace structures
publisher Virginia Tech
publishDate 2014
url http://hdl.handle.net/10919/36617
http://scholar.lib.vt.edu/theses/available/etd-32298-85910/
work_keys_str_mv AT hanuskaalexanderrobertjr thermalcharacterizationofcomplexaerospacestructures
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