Graduation Semester and Year

2015

Language

English

Document Type

Dissertation

Degree Name

Doctor of Philosophy in Aerospace Engineering

Department

Mechanical and Aerospace Engineering

First Advisor

Wen Chan

Abstract

Several studies have focused on the modeling and response characterization of composite structural members, with particular emphasis on thin-walled cylindrical composite shells. This class of shell configurations is explored to determine their mechanical response in primary aerospace structural members. The present work is focused on formulating a modified composite shell theory prognosis methodology for investigating the structural response of thin-walled cylindrical shell type composite configurations under axial and bending loads, respectively. The prime motivation to develop this theory arises from its capability to generate simple yet accurate closed-form analytical results that can efficiently charecterize cylindrical composite shell constructions. This work shows the development of a novel mathematical framework to predict key structural characteristics such as axial stiffness, bending stiffness, and centroid for thin walled composite shells. Longitudinal components of ply-stresses are analytically computed through the global stiffness matrix model for cylindrical composite tubes under thermomechanical environments. An ANSYS based FE routine is employed to compare against the analytical results. This concept development is further extended to analyze thin-walled, open cross-section, curved composite shells characterized by circumferential v arc angle, thickness-to-mean radius ratio, and total laminate thickness, respectively. The potential of this methodology is used to analytically identify the location of the centroid for such cross-sections. Ply stress variations for curved cylindrical shells are analytically examined under the application of centroidal tensile and bending loadings respectively. In-plane ply-stress estimations determined by the present model show excellent agreement in comparison with FEM results. The present work also incorporates the design and manufacturing of a novel ad-hoc testfixture set-up to experimentally characterize the extension-bending behavior in open cross-section curved composite strips. Seven symmetric, balanced curved composite test specimens are fabricated. This investigation introduces a new testing methodology to measure longitudinal surface strain fields and predict the centroid location via implementing a non-contact, full field strain measurement technique, Digital Image Correlation (DIC). Experimental measurements are compared against analytical results. This work is shown to essentially capture the mechanical response of cylindrical shells by providing an efficient and effective mathematical tool for structural engineers.

Disciplines

Aerospace Engineering | Engineering | Mechanical Engineering

Comments

Degree granted by The University of Texas at Arlington

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