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<title>Mechanical Engineering Faculty Works</title>
<copyright>Copyright (c) 2013 Loyola Marymount University and Loyola Law School All rights reserved.</copyright>
<link>http://digitalcommons.lmu.edu/mech_fac</link>
<description>Recent documents in Mechanical Engineering Faculty Works</description>
<language>en-us</language>
<lastBuildDate>Mon, 28 Jan 2013 23:25:11 PST</lastBuildDate>
<ttl>3600</ttl>








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<title>Applicability of Nanofluids in High Flux Solar Collectors</title>
<link>http://digitalcommons.lmu.edu/mech_fac/22</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/22</guid>
<pubDate>Thu, 09 Feb 2012 12:05:40 PST</pubDate>
<description>
	<![CDATA[
	<p>Concentrated   solar energy has become the input for an increasing number of experimental   and commercial thermal systems over the past 10-15 years [M.   Thirugnanasambandam et al., Renewable Sustainable Energy Rev. 14 (2010)].   Recent papers have indicated that the addition of nanoparticles to   conventional working fluids (i.e., nanofluids) can improve heat transfer and   solar collection [H. Tyagi et al., J. Sol. Energy Eng. 131, 4 (2009); P. E.   Phelan et al., Annu. Rev. Heat Transfer 14 (2005)]. This work indicates that   power tower solar collectors could benefit from the potential efficiency   improvements that arise from using a nanofluid working fluid. A notional   design of this type of nanofluid receiver is presented. Using this design, we   show a theoretical nanofluid enhancement in efficiency of up to 10% as   compared to surface-based collectors when solar concentration ratios are in   the range of 100-1000. Furthermore, our analysis shows that graphite   nanofluids with volume fractions on the order of 0.001% or less are suitable   for 10-100 MW(e) power plants. Experiments on a laboratory-scale nanofluid   dish receiver suggest that up to 10% increase in efficiency is possible   (relative to a conventional fluid)-if operating conditions are chosen   carefully. Lastly, we use these findings to compare the energy and revenue   generated in a conventional solar thermal plant to a nanofluid-based one. It   is found that a 100 MW(e) capacity solar thermal power tower operating in a   solar resource similar to Tucson, AZ, could generate similar to$ 3.5 million   more per year by incorporating a nanofluid receiver. (C) 2011 American   Institute of Physics. [doi: 10.1063/1.3571565]</p>

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<author>R. A. Taylor et al.</author>


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<title>Nanofluid-Based Direct Absorption Solar Collector</title>
<link>http://digitalcommons.lmu.edu/mech_fac/21</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/21</guid>
<pubDate>Thu, 09 Feb 2012 12:05:39 PST</pubDate>
<description>
	<![CDATA[
	<p>Solar   energy is one of the best sources of renewable energy with minimal   environmental impact. Direct absorption solar collectors have been proposed   for a variety of applications such as water heating; however the efficiency   of these collectors is limited by the absorption properties of the working   fluid, which is very poor for typical fluids used in solar collectors. It has   been shown that mixing nanoparticles in a liquid (nanofluid) has a dramatic   effect on the liquid thermophysical properties such as thermal conductivity.   Nanoparticles also offer the potential of improving the radiative properties   of liquids, leading to an increase in the efficiency of direct absorption   solar collectors. Here we report on the experimental results on solar   collectors based on nanofluids made from a variety of nanoparticles (carbon   nanotubes, graphite, and silver). We demonstrate efficiency improvements of   up to 5% in solar thermal collectors by utilizing nanofluids as the   absorption mechanism. In addition the experimental data were compared with a   numerical model of a solar collector with direct absorption nanofluids. The   experimental and numerical results demonstrate an initial rapid increase in   efficiency with volume fraction, followed by a leveling off in efficiency as   volume fraction continues to increase.</p>

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<author>Todd Otanicar et al.</author>


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<title>Nanofluid Optical Property Characterization: Towards Efficient Direct Absorption Solar Collectors</title>
<link>http://digitalcommons.lmu.edu/mech_fac/20</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/20</guid>
<pubDate>Thu, 09 Feb 2012 12:05:38 PST</pubDate>
<description>
	<![CDATA[
	<p>Suspensions   of nanoparticles (i.e., particles with diameters < 100 nm) in liquids,   termed nanofluids, show remarkable thermal and optical property changes from   the base liquid at low particle loadings. Recent studies also indicate that   selected nanofluids may improve the efficiency of direct absorption solar   thermal collectors. To determine the effectiveness of nanofluids in solar   applications, their ability to convert light energy to thermal energy must be   known. That is, their absorption of the solar spectrum must be established.   Accordingly, this study compares model predictions to spectroscopic   measurements of extinction coefficients over wavelengths that are important   for solar energy (0.25 to 2.5 mu m). A simple addition of the base fluid and nanoparticle   extinction coefficients is applied as an approximation of the effective   nanofluid extinction coefficient. Comparisons with measured extinction   coefficients reveal that the approximation works well with water-based   nanofluids containing graphite nanoparticles but less well with metallic   nanoparticles and/or oil-based fluids. For the materials used in this study,   over 95% of incoming sunlight can be absorbed (in a nanofluid thickness >=   10 cm) with extremely low nanoparticle volume fractions - less than 1 x   10(-5), or 10 parts per million. Thus, nanofluids could be used to absorb   sunlight with a negligible amount of viscosity and/or density (read: pumping   power) increase.</p>

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<author>R. A. Taylor et al.</author>


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<title>Evaluation of the Effects of Powder Coating Cure Temperatures on the Mechanical Properties of Aluminum Alloy Substrates</title>
<link>http://digitalcommons.lmu.edu/mech_fac/19</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/19</guid>
<pubDate>Thu, 09 Feb 2012 11:56:21 PST</pubDate>
<description>
	<![CDATA[
	<p>The   effects of curing temperature, based on new, low-temperature powder coating   methods and traditional high-temperature powder coating methods, were   studied. Heat-sensitive aluminum alloys (2024-T3, 6061-T6, and 7075-T6) were   subjected to two different heat-treatment cycles, which were based on   temperatures of 121 and 204 degrees C. Findings indicate that although both   cure temperatures achieved powder coatings adhesion and thickness appropriate   for industrial uses, the high-temperature cure treatment negatively affected   the mechanical properties.</p>

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<author>C. Maldonado et al.</author>


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<title>Innovative Manufacturing Process for Defect Free, Affordable, High Pressure, Thin Walled, Hydraulic Tubing</title>
<link>http://digitalcommons.lmu.edu/mech_fac/18</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/18</guid>
<pubDate>Thu, 09 Feb 2012 11:56:11 PST</pubDate>
<description>
	<![CDATA[
	<p>Various   thermo-mechanical processes were performed on a standard and a low oxygen   content Ti-6Al-4V alloy. Testing was performed to determine whether it was   possible to achieve a combination of tensile properties comparable to those   of Ti-3Al-2.5V by means of cold working and annealing Ti-6Al-4V from a   thickness of 0.671 cm (0.264 in.) to that between 0.081 and 0.094 cm   (0.032-0.037 in.), which had never been carried out before. The resulting   mechanical properties of this study were compared to the mechanical   properties of Ti-3Al-2.5V to determine whether Ti-6Al-4V could be used as a   suitable replacement for hydraulic tubing applications. The optimum results   were achieved with 10-15% cold work and annealing at 750 A degrees C (1382 A   degrees F) for 2 h between cold work reductions in thickness. It was   concluded that Ti-6Al-4V was a suitable replacement for Ti-3Al-2.5V for   hydraulic tubing with an increase in ultimate and yield strengths, but with a   slight sacrifice of 5-10% elongation.</p>

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<author>W. Miranda et al.</author>


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<title>Microstructure Analysis of Aluminum Alloy and Copper Alloy Circular Shells After Multiaxial Plastic Buckling</title>
<link>http://digitalcommons.lmu.edu/mech_fac/17</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/17</guid>
<pubDate>Thu, 09 Feb 2012 11:55:56 PST</pubDate>
<description>
	<![CDATA[
	<p>Aluminum   and copper cylindrical shells were plastically buckled under quasi-static and   dynamic loading conditions with an Absorption Compression-Torsion Plasticity   (ACTP: Patent No. WO 2005090822) combined mechanical testing device. Optical   microscopy and transmission electron microscopy (TEM) analysis were used to   study the microscopic evolutions in the mechanically buckled aluminum and   copper alloy samples. Optical microscopy showed evidence of the presence of   second-phase particles in both the aluminum and copper alloys samples. Under   dynamic loading aluminum samples showed more energy absorption as compared to   copper samples. Material flow lines were more pronounced in the copper   samples when observed by optical microscopy. The evidence that supports the   increased energy absorption in the aluminum cylindrical shells can be   supported by the TEM analysis more than the optical microscopy analysis. The   TEM results showed highly oriented textured morphology with the presence of   few dislocation cells structures and sub-structures.</p>

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<author>N. Drusina et al.</author>


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<title>On the Distortion and Warpage of 7249 Aluminum Alloy After Quenching and Machining</title>
<link>http://digitalcommons.lmu.edu/mech_fac/16</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/16</guid>
<pubDate>Thu, 09 Feb 2012 11:55:32 PST</pubDate>
<description>
	<![CDATA[
	<p>The   objective of this study is to determine the effect of solution treatment   temperature, quenching media, and various machining sequences on the warpage   behavior of aluminum 7249 alloy aged to T6 and T7' tempers. Large extrusions   of 7249 aluminum alloy with fins were cut into 108 "T" sections.   The samples were solution-treated, aged, and machined. Three solution   temperatures (445, 474, and 505 A degrees C), two quenching media (water and   20% polyalkylene glycol), two aging treatments (T6 and T7'), and three   machine sequences were used. The flatness of the samples was measured on the   surfaces orthogonal to the z-axis. Three points were on top of both shoulders   (six total), six were at the bottom of the sample, and six were on the top of   the fin, in the cases where the fin was not milled off. They were then   averaged together by surface to represent the overall warpage of each sample.</p>

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<author>N. Keleshian et al.</author>


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<title>Tensile Properties and Microstructures of Laser-Formed Ti-6Al-4V</title>
<link>http://digitalcommons.lmu.edu/mech_fac/15</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/15</guid>
<pubDate>Thu, 09 Feb 2012 11:55:03 PST</pubDate>
<description>
	<![CDATA[
	<p>The room   temperature tensile properties of Ti-6Al-4V alloy prepared under two   different processing routes were evaluated and compared. One group of samples   was prepared by conventional casting-forging-rolling into flat plates. The   other group was prepared by using Triton's Laser Free-Form Fabrication   (LF3)(TM) processes, i.e., a laser was used to melt pre-alloyed powders of   the required metallic composition as they were dropped onto a moveable   substrate programmed to move in such a manner as to form a solid alloy plate.   Five populations of Ti-6Al-4V were evaluated: a standard wrought form, an   as-deposited form, a machined as-deposited form, a heat-treated as-deposited   form, and a machined as-deposited and heat-treated form. The poorest   mechanical properties occurred with the rough surfaces, likely due to   existing microcracks and stress concentrations. The LF3 (TM) as-deposited   material had mechanical properties comparable to, if not higher than, the   mechanical properties of the wrought material. Further evaluations of the   laser-formed material for complex spacecraft piece parts were warranted,   specifically in regards to improving the surface finish of the materials.</p>

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<author>J. Alcisto et al.</author>


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<title>The Effect of Layer Orientation on the Mechanical Properties and Microstructure of a Polymer</title>
<link>http://digitalcommons.lmu.edu/mech_fac/14</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/14</guid>
<pubDate>Thu, 09 Feb 2012 11:54:17 PST</pubDate>
<description>
	<![CDATA[
	<p>Rapid   Prototyping (RP) is a method used everywhere from the entertainment industry   to healthcare. Layer orientation is an important aspect of the final product.   The objective of this research was to evaluate the effect of layer   orientation on the mechanical strength and toughness of a polymer. The   polymer used was a combination of two materials, ZP 130 and ZB 58, fused   together in the Z Corporation Spectrum Z510 Rapid Prototyping Machine. ZP 130   is a powder composed of vinyl polymer (2-20%), sulfate salt (0-5%), and   plaster that contains < 1% crystalline silica (50-95%). ZB 58 is a liquid   composed of glycerol (1-10%), preservative (sorbic acid salt) (0-2%),   surfactant (< 1%), pigment (< 1%), and water (85-95%). After removal   from the machine the samples were sealed with Z bond 101 which is   Beta-methoxyethyl cyanoacrylate (60-100%). The layer orientations studied   were the crack arrestor, crack divider, and short transverse with various   combinations of the three, for a total of seven orientations. The mechanical   strength was evaluated using tensile testing and three-point bend testing.   The toughness was evaluated by Izod impact testing. Five samples for tensile   testing and three-point bend testing as well as 15 samples for the Izod   impact test for each of the seven orientations were made. The total number of   samples was 175. The crack arrestor orientation was the strongest main   orientation for the tensile and three-point bend test. Weibull analysis was   done on the Izod impact testing due to high variation in the results for the   crack arrestor and short transverse directions. It was found that the layer   orientation and surface roughness played a significant role in the   penetration of the Z bond 101 coating and in the overall strength of the samples.</p>

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<author>V. Vega et al.</author>


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<title>The Effects of Retrogression and Reaging on Aluminum Alloy 2099 (C458)</title>
<link>http://digitalcommons.lmu.edu/mech_fac/13</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/13</guid>
<pubDate>Thu, 09 Feb 2012 11:53:35 PST</pubDate>
<description>
	<![CDATA[
	<p>The   objective of this study was to investigate the feasibility of performing   retrogression and reaging (RRA) heat treatments on 2099 aluminum-lithium   alloy. The retrogression temperatures were 200-250 A degrees C and   retrogression times were 5-60 min. Half of the samples were exposed to a salt   fog environment. Interestingly, the samples exposed to salt spray had   consistently higher mechanical tensile properties than those which were not   exposed.</p>

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<author>N. Ward et al.</author>


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<title>The Effects of Retrogression and Reaging on Aluminum Alloy 2195</title>
<link>http://digitalcommons.lmu.edu/mech_fac/12</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/12</guid>
<pubDate>Thu, 09 Feb 2012 11:51:25 PST</pubDate>
<description>
	<![CDATA[
	<p>A   retrogression and reaging (RRA) treatment was performed on 2195 Al-Li Alloy.   The exposure times were from 5 to 60 min, and the temperatures were from 200   to 250 A degrees C. Samples that were exposed to a salt spray test had   overall similar mechanical properties as compared to those that were not   exposed. The percent elongation, however, was significantly deteriorated due   to the salt spray exposure. The mechanical properties of the 2195 samples   were compared to those of 2099 samples exposed to similar treatments in an   earlier study.</p>

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<author>N. Ward et al.</author>


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<title>Vapor Generation in a Nanoparticle Liquid Suspension Using a Focused, Continuous Laser</title>
<link>http://digitalcommons.lmu.edu/mech_fac/11</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/11</guid>
<pubDate>Thu, 09 Feb 2012 11:48:49 PST</pubDate>
<description>
	<![CDATA[
	<p>This   letter discusses experimentation with optically induced phase change in   nanoparticle liquid suspensions-commonly termed nanofluids. Four different   types of nanofluids at five concentrations were exposed to a similar to 120   mW, 532 nm laser beam to determine the minimum laser flux needed to create   vapor. Laser irradiance was varied between 0-770 W cm(-2). While the   experiments were simple, they involved many complex, interrelated physical   phenomena, including: subcooled boiling, thermal driven particle/bubble   motion, nanoparticle radiative absorption/scattering, and nanoparticle   clumping. Such phenomena could enable novel solar collectors in which the   working fluid directly absorbs energy and undergoes phase change in a single   step. c 2009 American Institute of Physics. [doi: 10.1063/1.3250174]</p>

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<author>R. A. Taylor et al.</author>


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<title>Parametric Analysis of a Coupled Photovoltaic/Thermal Concentrating Solar Collector for Electricity Generation</title>
<link>http://digitalcommons.lmu.edu/mech_fac/10</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/10</guid>
<pubDate>Thu, 09 Feb 2012 11:45:52 PST</pubDate>
<description>
	<![CDATA[
	<p>The   analysis of the combined efficiencies in a coupled photovoltaic (PV)/thermal   concentrating solar collector are presented based on a coupled   electrical/thermal model. The calculations take into account the drop in   efficiency that accompanies the operation of PV cells at elevated   temperatures along with a detailed analysis of the thermal system including   losses. An iterative numerical scheme is described that involves a coupled   electrothermal simulation of the solar energy conversion process. In the proposed   configuration losses in the PV cell due to reduced efficiencies at elevated   temperatures and the incident solar energy below the PV bandgap are both   harnessed as heat. This thermal energy is then used to drive a thermodynamic   power cycle. The simulations show that it is possible to optimize the overall   efficiency of the system by variation in key factors such as the solar   concentration factor, the band gap of the PV material, and the system thermal   design configuration, leading to a maximum combined efficiency of similar to   32.3% for solar concentrations between 10-50 and a band-gap around 1.5-2.0   eV. (C) 2010 American Institute of Physics. [doi: 10.1063/1.3514590]</p>

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<author>Todd Otanicar et al.</author>


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<title>High-Resolution Methods for Measuring the Thermal Expansion Coefficient of Aerospace Materials</title>
<link>http://digitalcommons.lmu.edu/mech_fac/9</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/9</guid>
<pubDate>Thu, 09 Feb 2012 10:51:41 PST</pubDate>
<description>
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	<p>Accurately   predicting the coefficient of thermal expansion for many aerospace components   is critical to ensure proper functionality on orbit where the temperature   gradient across a spacecraft can vary from +300 degrees F to -450 degrees F.   Under these conditions, the linear approximations generated by theoretical   equations no longer hold true, and experimental methods are needed. Although   several methods exist for measuring the coefficient of thermal expansion of   materials, laser interferometry yields high-resolution results, and the   technique is widely accepted in the scientific community.</p>

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<author>G. Wallace et al.</author>


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<title>The Effect of Thermal Exposure on the Mechanical Properties of 2099-T6 Die Forgings, 2099-T83 Extrusions, 7075-T7651 Plate, 7085-T7452 Die Forgings, 7085-T7651 Plate, and 2397-T87 Plate Aluminum Alloys</title>
<link>http://digitalcommons.lmu.edu/mech_fac/8</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/8</guid>
<pubDate>Thu, 09 Feb 2012 10:51:39 PST</pubDate>
<description>
	<![CDATA[
	<p>Aluminum   alloys 2099-T6 die forgings, 2099-T83 extrusions, 7075-T7651 plate,   7085-T7452 die forgings, 7085-T7651 plate, and 2397-T87 plate were thermally   exposed at temperatures of 180 degrees C (350 degrees F), 230 degrees C (450   degrees F), and 290 degrees C (550 degrees F) for 0.1, 0.5, 2, 10, 100, and   1000 h. The purpose of this study was to determine the effect of thermal   exposure on the mechanical properties and electrical conductivity of these   alloys. The data shows that higher temperatures and longer exposure times   generally resulted in decreased strength and hardness and increased percent   elongation and electrical conductivity.</p>

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<author>J. Jabra et al.</author>


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<title>Analysis of Heat Effects on Marine Corps AM2 Mat Mechanical Properties</title>
<link>http://digitalcommons.lmu.edu/mech_fac/7</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/7</guid>
<pubDate>Thu, 09 Feb 2012 10:51:38 PST</pubDate>
<description>
	<![CDATA[
	<p>Navy AM2   mats are used as portable aircraft landing platforms for the Short   Take-off/Vertical Landing (STOVL) aircraft operations. This investigation   presents the study performed to determine whether the surface discoloration   is a precursor to degradation in the mechanical property of the AM2 mat   material. The red discoloration on the mat surfaces had a clear correlation   with the decrease in yield strength, ultimate strength, and hardness   properties.</p>

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<author>V. Vega et al.</author>


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<title>Warpage Behavior of 7075 Aluminum Alloy Extrusions</title>
<link>http://digitalcommons.lmu.edu/mech_fac/6</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/6</guid>
<pubDate>Thu, 09 Feb 2012 10:50:57 PST</pubDate>
<description>
	<![CDATA[
	<p>Extruded   I sections of 7075-T6 aluminum were machined into four different sections   shapes: L, short depth L, T, and short depth 7. The furnace was preheated to   416 degrees C (780 degrees F) and the samples were placed inside. The   temperature was raised to 471 degrees C (880 degrees F) and then the samples   were quenched in either a 30% polyalkylene Glycol solution or water, both at   15 degrees C (59 degrees F). Points on the distorted samples were recorded   before and after the solution treatment; the difference between the   measurements indicated the extent of warpage.</p>

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<author>Omar S. Es-Said et al.</author>


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<title>Effect of Stretch Orientation and Rolling Orientation on the Mechanical Properties of 2195 Al-Cu-Li Alloy</title>
<link>http://digitalcommons.lmu.edu/mech_fac/5</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/5</guid>
<pubDate>Thu, 09 Feb 2012 10:50:56 PST</pubDate>
<description>
	<![CDATA[
	<p>Sheets of   2195 aluminum-lithium alloy were solution-treated at 507 A degrees C for 30   min. One set was stretched to 3-5% in the 0A degrees, 45A degrees, and 90A   degrees angle with respect to the original rolling direction. Two other sets   were rolled 6% reduction in thickness and 24% reduction in thickness in the   0A degrees, 45A degrees, and 90A degrees angle with respect to the original   rolling direction. All specimens were aged at 143 A degrees C for 36 h. A   second group of samples was rolled at 24 and 50% reduction in thickness after   a solution treatment of 507 A degrees C for 1 h prior to aging at 190 A   degrees C for 24 h. Tensile specimens were machined from each sheet at 0A   degrees, 45A degrees, and 90A degrees angles to the original grain orientation.   Tensile testing was used to determine the mechanical properties and   anisotropic behavior of each condition. Rolling 6% reduction in thickness in   the 45A degrees orientation yielded anisotropy of 7.6% in the yield strength.</p>

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<author>Omar S. Es-Said et al.</author>


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<title>Evaluation of Advanced Adhesives for Aerospace Structures</title>
<link>http://digitalcommons.lmu.edu/mech_fac/4</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/4</guid>
<pubDate>Thu, 09 Feb 2012 10:50:54 PST</pubDate>
<description>
	<![CDATA[
	<p>Polymer   adhesives are finding increased use in panel joining applications in aircraft   and aerospace structures where the applied stresses permit their use and   where a uniform stress distribution is needed. One such adhesive, Hysol   EA-9394 (TM), was compared to three other formulations in this study. The new   formulations were Hysol EA-9396, Hysol EA-9396 filled with nickel nanofibers   and mixed by machine (Jamesbury Blender), and Hysol EA-9396 filled with   nickel nanofibers and hand mixed in the laboratory. The comparison consisted   of measuring shear lap strengths of aluminum test pieces bonded together with   the candidate adhesives. The mechanical tests were supplemented by a Weibull   analysis of the strength data and by a visual inspection of the failure mode   (adhesive/cohesive). The lap shear strengths (fracture stress values) of all   three Hysol EA-9396 adhesives were greater than that of the baseline Hysol   EA-9394 polymer.</p>

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<author>P. Stoyanov et al.</author>


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<title>Effect of Cold Work on the Tensile Properties of 6061, 2024, and 7075 Al Alloys</title>
<link>http://digitalcommons.lmu.edu/mech_fac/3</link>
<guid isPermaLink="true">http://digitalcommons.lmu.edu/mech_fac/3</guid>
<pubDate>Thu, 09 Feb 2012 10:11:29 PST</pubDate>
<description>
	<![CDATA[
	<p>Aluminum   alloys 6061, 2024, and 7075 were heat treated to various tempers and then   subjected to a range of plastic strain (stretching) in order to determine   their strain limits. Tensile properties, conductivity, hardness, and grain   size measurements were evaluated. The effects of the plastic strain on these   properties are discussed and strain limits are suggested.</p>

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<author>D. Ortiz et al.</author>


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