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    <title>DSpace collection: ME Graduate Student Conference Papers</title>
    <link>http://hdl.handle.net/10057/179</link>
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    <item>
      <title>Effect of cutting temperatures on the hole quality of a carbon-fiber composite</title>
      <link>http://hdl.handle.net/10057/1360</link>
      <description>title: Effect of cutting temperatures on the hole quality of a carbon-fiber composite authors: Rahman, Khan Habeeb Ur; Bahr, Behnam
&lt;br&gt;abstract: The drilling of composites project is aimed at minimizing delamination and reducing the fiber pull out, thereby&#xD;
improving the hole quality. The heat generated during drilling has an adverse effect on the hole quality. So it is important to&#xD;
analyze the effect of cutting temperatures on the dimensional accuracy of the drilled hole namely hole oversize and&#xD;
roundness and also its effect on the surface finish/roughness of the drilled hole. The drill bit will also be tested for the same&#xD;
parameters using a mist cooling system. These results will be compared with one another. Also the results of different drill&#xD;
bits will be compared with one another.
&lt;br&gt;description: Paper presented to the 4th Annual Symposium on Graduate Research and Scholarly Projects (GRASP) held at the Hughes Metropolitan Complex, Wichita State University, April 25, 2008.
&lt;br&gt;</description>
      <pubDate>Thu, 24 Apr 2008 22:58:59 GMT</pubDate>
    </item>
    <item>
      <title>Investigation of the effect of different parameters in the drilled hole quality in composite materials</title>
      <link>http://hdl.handle.net/10057/919</link>
      <description>title: Investigation of the effect of different parameters in the drilled hole quality in composite materials authors: Sahraie Jahromi, Ashkan; Rahman, Khan Habeeb Ur; Bassi, R.; Bahr, Behnam
&lt;br&gt;abstract: Two different delamination mechanisms that&#xD;
need to be controlled by the drill geometry and thrust force&#xD;
will be observed in the drilling of composites. The studies&#xD;
which have been done up to now focus on the thrust force&#xD;
aspect and drill bit geometry at a constant feed rate.&#xD;
It is possible to find a feed rate at the beginning of the&#xD;
penetration that corresponds to the rate at which the&#xD;
laminates are peeled out. Moreover, at the exit, the fiber&#xD;
push-down mechanism is active, which can be controlled&#xD;
by controlling the maximum thrust force. Thrust force itself&#xD;
depends on the feed rate, so there should be a “feed ratedepth”&#xD;
graph minimizing the delamination. This implies&#xD;
that the feed rate may need to be changed from high to low&#xD;
as the drill bit enters and exits. To find the best result&#xD;
several experiments are being run at the constant feed rate.&#xD;
Some of these feed rates will give reduced fiber pull outs at&#xD;
the entrance and some will result in acceptable fiber push&#xD;
downs at the exit. The best graph will be extracted by&#xD;
analyzing the delamination for each feed rate. For&#xD;
measuring, a microscope should be used to determine the&#xD;
areas with the maximum delamination along the cross&#xD;
section of the hole. Also, measuring the surface roughness&#xD;
is another method of determining the delamination, but it&#xD;
should be done at a certain depth at the entrance as well as&#xD;
exit, not all of the thickness at once. [1]
&lt;br&gt;description: Paper presented to the 3rd Annual Symposium on Graduate Research and Scholarly Projects (GRASP) held at the Hughes Metropolitan Complex, Wichita State University, April 27, 2007.
&lt;br&gt;</description>
      <pubDate>Thu, 26 Apr 2007 22:58:59 GMT</pubDate>
    </item>
    <item>
      <title>Determination of damage area of spacecraft shields impacted by space debris at hypervelocity using an SPH mesh.</title>
      <link>http://hdl.handle.net/10057/918</link>
      <description>title: Determination of damage area of spacecraft shields impacted by space debris at hypervelocity using an SPH mesh. authors: Bhargavi, S.S.; Soschinske, Kurt A.; Lankarani, Hamid M.
&lt;br&gt;abstract: Space debris, are objects in Earth orbit consisting of small fragments from spent rocket stages and non-functional&#xD;
satellites. Accumulated in the lower earth orbit, these often cause considerable damage to the spacecraft orbiting around the earth.&#xD;
Hence it’s necessary to develop ways to protect the newly placed spacecraft from the debris. The goal of the project was to&#xD;
determine the damage area of the pressure wall using the Smoothed Particle Hydrodynamic (SPH) meshing, a dynamic finite&#xD;
element modeling (FEM) method.
&lt;br&gt;description: Paper presented to the 3rd Annual Symposium on Graduate Research and Scholarly Projects (GRASP) held at the Hughes Metropolitan Complex, Wichita State University, April 27, 2007.
&lt;br&gt;</description>
      <pubDate>Thu, 26 Apr 2007 22:58:59 GMT</pubDate>
    </item>
    <item>
      <title>Crevice corrosion theory, mechanisms and prevention methods</title>
      <link>http://hdl.handle.net/10057/917</link>
      <description>title: Crevice corrosion theory, mechanisms and prevention methods authors: Rashidi, Navid; Alavi-Soltani, Seyed R.; Asmatulu, Ramazan
&lt;br&gt;abstract: This paper reviews theory and mechanisms of&#xD;
crevice corrosion as well as its prevention methods. Crevice&#xD;
corrosion is one of the most important and harmful forms of&#xD;
localized corrosion that may cause sudden failure of the metal&#xD;
in service if not prevented properly. So far several protection&#xD;
methods against crevice corrosion have been developed&#xD;
including cathodic protection and using inhibitors and&#xD;
coatings. Hot wax dip method and sealing crevices with&#xD;
polysulfide are two popular protection methods currently&#xD;
used in automotive and aerospace industries respectively.&#xD;
However researches about this devastating type of corrosion&#xD;
still continue.
&lt;br&gt;description: Paper presented to the 3rd Annual Symposium on Graduate Research and Scholarly Projects (GRASP) held at the Hughes Metropolitan Complex, Wichita State University, April 27, 2007.
&lt;br&gt;</description>
      <pubDate>Thu, 26 Apr 2007 22:58:59 GMT</pubDate>
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