Aerospace Engineering
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AE Faculty Selected Works [53]
Collection of Aerospace Engineering faculty research publications
Collections in this community
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AE Graduate Student Conference Papers [47]
Aerospace Engineering graduate students GRASP papers and abstracts -
AE Research Publications [99]
Research publications authored by the Department of Aerospace Engineering faculty and graduate students. -
AE Theses and Dissertations [134]
Electronic copies of theses and dissertations defended in the Department of Aerospace Engineering
Recent Submissions
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Elastic-plastic analysis of adhesive-bonded single-lap composite joints under tension
(American Society of Mechanical Engineers(ASME), 1993-07)An analytical model of adhesive-bonded single-lap composite joints is developed to predict the stress-strain distributions with such joints under tensile loading. The First-order laminated anisotropic plate theorem is ... -
Impact response and microstructural analysis of two glass/epoxy composite laminates
(American Society of Mechanical Engineers (ASME), 1995-06)Low velocity impact tests were performed on two glass/epoxy (spring orientation and crossply) composite laminates. A weight drop tower tester was previously constructed to study the impact energy absorbed by a composite ... -
Strength analysis of butt and strap joints under tension and bending
(Society for the Advancement of Material and Process Engineering, 1990-04)The strength analysis of a butt and strap composite pipe joint is provided. This commercial joint consists of mating two sections of pipe and overwrapping them with additional composite laminae. The pipe analyzed in this ... -
Qualification of advanced composite pipe for use in fire water deluge systems on open type offshore oil platforms
(American Society of Mechanical Engineers (ASME), 1996-07)Different types of FIBERBOND pipe in the dry condition and with a butt & strap joint were subjected to a controlled fire for fire endurance evaluation. Testing adheres to a modification of the ASTM 1173-95 guideline, which ... -
Stress-strain analysis of an adhesive-bonded taper-taper joint between two composite flat plates
(Society of Plastics Engineers (SPE), 1996-05)An analytical model of a taper-taper adhesive-bonded joint between two composite flat plates has been developed using classical first-order laminated plate theory and including a correction for transverse shear deformation ... -
Strength analysis of adhesive-bonded single-lap composite joints
(American Society of Mechanical Engineers(ASME), 2001-02)An analytical model was developed to determine the stress and strain distributions of adhesive-bonded composite single-lap joints under tension. Laminated anisotropic plate theory was applied in the derivation of the ... -
Analytical modeling of ASTM lap shear adhesive specimens. FInal report
(National Technical Information Service (NTIS), 2003-02)An analytical model was developed to predict the stress distribution within the specimen specified in ASTM D 3165 Strength Properties of Adhesives in Shear by Tension Loading of Single-Lap-Joint Laminated Assemblies. In ... -
A numerical and experimental approach to characterize the failure modes of hexagonal cell honeycomb core under in-plane loading
(DEStech Publications Inc., 2017-10)In the present study, the failure modes of a hexagonal cell honeycomb core under in-plane loading are investigated. It is shown that, under tensile loading, the node bond failure and ribbon fracture are the main causes of ... -
Fracture analysis of adhesive-bonded single-lap composite joints
(Society for the Advancement of Material and Process Engineering, 2004-05)A fracture mechanics model to estimate the energy release rate of adhesive-bonded single-lap composite joints under tension has been developed. The stress distributions of the adhesive-bonded single-lap composite joint ... -
Stress-strain analysis of adhesive-bonded single-lap composite joints under cylindrical bending
(Elsevier, 1993)An analytical study is proposed to develop an advanced model for determining the stress and strain distributions of adhesive-bonded composite single-lap joints under cylindrical bending. The anisotropic laminated plate ... -
Calculation of strain energy release rates for bonded joints with a prescribed crack
(Woodhead Publishing Limited, 2011-10)This chapter provides two general approaches to calculate the strain energy release rate of adhesively bonded composite joints with a prescribedcrack. The general structural response of adhesively bonded composite joints ... -
Heat-activated joining technology for composite to alloy piping systems
(Society of Plastics Engineers (SPE), 1998-04)A new process for joining composite to alloy piping systems, the heat-activated joining technique, has been developed. The strength of the heat coupling joint in bending, tension, and hydro static testing was comparable ... -
Strain energy release rate analysis of adhesive-bounded composite laminate joints with a cohesive crack
(American Society for Composites (ASC) & Canadian Association Composites Structures and Materials (CACSMA), 2009-09)Fiber-reinforced composites have been widely used in the aviation industry due to their light weight and high corrosion resistance. In many applications, bolted joints have been replaced by adhesive-bonded joints because ... -
Experimental and numerical study on the mechanical response of fiberglass/phenolic honeycomb core under uniaxial in-plane loading
(Society for the Advancement of Material and Process Engineering (SAMPE), 2017-05)A series of in-plane quasi-static tensile and compressive tests are carried out on a Fiberglass/Phenolic hexagonal cell honeycomb core to characterize the uniaxial in-plane responses of the honeycomb core under large ... -
Analysis of in-plane mechanical response of hexagonal honeycomb core: Effect of node bond adhesive and proposed analytical method
(DEStech Publications Inc., 2017-10)In this study, the development of an analytical model to predict the homogenized in-plane stress-strain behavior of hexagonal honeycomb core under large deformations is presented. Unlike in traditional models, the detailed ... -
Strain energy release rate analysis of bonded structural composite joints with a prescribed crack
(Society for the Advancement of Material and Process Engineering (SAMPE), 2006)Advanced composite materials have been widely used due to their light weight and high corrosion resistance. In many of these applications, bolted joint shave been replaced by adhesively bonded joints because of the weight ... -
Improving the mechanical properties of composite pipe using multi-angle filament winding
(National Association of Corrosion Engineers International, 1998-03)The benefits of composite materials-light weight, corrosion resistance, handling ease, etc., have long been appreciated. Composite piping systems are gaining wide acceptance in various industries such as petrochemical, ... -
Strength model of adhesive bonded double lap joints under cantilevered bending
(Society of Plastics Engineers (SPE), 1992-05)The objective of this study was to develop mathematical relations for predicting the strength of adhesive?bonded double?lap joints under cantilevered bending. Based on the strength of composite materials theory, two models ... -
Investigation of thick bondline adhesive joints. FInal report
(National Technical Information Service (NTIS), 2001-06)In recent years, the use of polymer matrix composite materials as primary structural components has risen, especially in the general aviation (GA) industry. The use of composites not only results in weight savings, but ... -
Investigation of adhesive behavior in aircraft applications
(National Technical Information Service (NTIS), 2001-09)There are two parts included in this report. The first part evaluates the most commonly used test method for adhesive properties, ADTM D 5656 Standard Test Method for Thick-Adherend Metal Lap-Shear Joints for Determination ...
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