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<title>MaterialPedia - The five questions posted most recently:</title>
<description>Material encyclopedia</description>
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		<title><![CDATA[Tensile test and Strain-Stress Diagram]]></title>
		<description><![CDATA[<p>
Tensile test and Strain-Stress Diagram<br />
<br />
Strain-Stress Diagram expresses a relationship between a load applied to a material and the deformation of the material, caused by the load .
</p>
<p>
<br />
<br />
Strain-Stress Diagram is determined by tensile test.<br />
<br />
Tensile tests are conducted in tensile test machines, providing controlled uniformly increasing tension force, applied to the specimen.<br />
<br />
The specimen’s ends are gripped and fixed in the machine and its gauge length L0 (a calibrated distance between two marks on the specimen surface) is continuously measured until the rupture.<br />
<br />
Test specimen may be round or flat in the cross-section.<br />
<br />
In the round specimens it is accepted, that L0 = 5 * diameter.<br />
<br />
The specimen deformation (strain) is the ratio of the increase of the specimen gauge length to its original gauge length:<br />
<br />
&#948; = (L – L0) / L0<br />
<br />
Tensile stress is the ratio of the tensile load F applied to the specimen to its original cross-sectional area S0:<br />
<br />
&#963; = F / S0<br />
<br />
tensile specimen.png<br />
<br />
The initial straight line (0P)of the curve characterizes proportional relationship between the stress and the deformation (strain).<br />
<br />
The stress value at the point P is called the limit of proportionality:<br />
<br />
&#963;p= FP / S0<br />
<br />
This behavior conforms to the Hook’s Law:<br />
<br />
&#963; = E*&#948;<br />
<br />
Where E is a constant, known as Young’s Modulus or Modulus of Elasticity.<br />
<br />
The value of Young’s Modulus is determined mainly by the nature of the material and is nearly insensitive to the heat treatment and composition.<br />
<br />
Modulus of elasticity determines stiffness - resistance of a body to elastic deformation caused by an applied force.<br />
<br />
The line 0E in the strain-stress curve indicates the range of elastic deformation – removal of the load at any point of this part of the curve results in return of the specimen length to its original value.<br />
<br />
The elastic behavior is characterized by the elasticity limit (stress value at the point E):<br />
<br />
&#963;el= FE / S0<br />
<br />
For the most materials the points P and E coincide and therefore &#963;el=&#963;p.<br />
<br />
strain-stress diagram.png<br />
<br />
<br />
A point where the stress causes sudden deformation without any increase in the force is called yield limit (yield stress, yield strength):<br />
<br />
&#963;y= FY / S0<br />
<br />
The highest stress (point YU) , occurring before the sudden deformation is called upper yield limit .<br />
<br />
The lower stress value, causing the sudden deformation (point YL) is called lower yield limit.<br />
<br />
The commonly used parameter of yield limit is actually lower yield limit.<br />
<br />
If the load reaches the yield point the specimen undergoes plastic deformation – it does not return to its original length after removal of the load.<br />
<br />
proof stress.png<br />
<br />
Hard steels and non-ferrous metals do not have defined yield limit, therefore a stress, corresponding to a definite deformation (0.1% or 0.2%) is commonly used instead of yield limit. This stress is called proof stress or offset yield limit (offset yield strength):<br />
<br />
&#963;0.2%= F0.2% / S0<br />
<br />
The method of obtaining the proof stress is shown in the picture.<br />
<br />
As the load increase, the specimen continues to undergo plastic deformation and at a certain stress value its cross-section decreases due to “necking” (point S in the strain-stress diagram). At this point the stress reaches the maximum value, which is called ultimate tensile strength (tensile strength):<br />
<br />
&#963;t= FS / S0<br />
<br />
Continuation of the deformation results in breaking the specimen - the point B in the diagram.<br />
<br />
The actual strain-stress curve is obtained by taking into account the true specimen cross-section instead of the original value.<br />
<br />
Other important characteristic of metals is ductility - ability of a material to deform under tension without rupture.<br />
<br />
Two ductility parameters may be obtain from the tensile test:<br />
<br />
Relative elongation - ratio between the increase of the specimen length before its rupture and its original length:<br />
<br />
&#948; = (Lm– L0) / L0<br />
<br />
Where Lm– maximum specimen length.<br />
<br />
Relative reduction of area - ratio between the decrease of the specimen cross-section area before its rupture and its original cross-section area:<br />
<br />
&#968;= (S0– Smin) / S0<br />
<br />
Where Smin– minimum specimen cross-section area.<br />
</p>
]]></description>
		<link>http://www.materialpedia.com/content/9/30/en/tensile-test-and-strain_stress-diagram.html</link>
		<pubDate>Thu, 29 May 2008 22:21:00 GMT</pubDate>
	</item>
	<item>
		<title><![CDATA[AISI SAE 5140]]></title>
		<description><![CDATA[<h1><a id="alloy_steel_sae_5140" name="alloy_steel_sae_5140"></a>Alloy steel SAE 5140</h1>
<p>
(submitted by the website administration)<br />
<br />
</p>
<table border="0" class="inline">
	<tbody>
		<tr>
			<td class="centeralign" colspan="5">  <strong>SAE 5140</strong>  </td>
		</tr>
		<tr>
			<td colspan="5"> <strong>Chemical composition: </strong>C=0.40%, Mn=0.8%, Cr=0.8% </td>
		</tr>
		<tr>
			<td> <strong>Property</strong> </td>
			<td colspan="2"> <strong>Value in metric unit</strong> </td>
			<td colspan="2"> <strong>Value in </strong><strong>US</strong><strong> unit</strong> </td>
		</tr>
		<tr>
			<th> Density </th>
			<td class="centeralign">  7.872 *10³  </td>
			<td> kg/m³ </td>
			<td class="centeralign">  491.4  </td>
			<td> lb/ft³ </td>
		</tr>
		<tr>
			<th> Modulus of elasticity </th>
			<td class="centeralign">  205  </td>
			<td> GPa </td>
			<td class="centeralign">  29700  </td>
			<td> ksi </td>
		</tr>
		<tr>
			<th> Thermal expansion (20 ºC) </th>
			<td class="centeralign">  12.6*10<sup>-6</sup>  </td>
			<td> ºC&#713;¹ </td>
			<td class="centeralign">  7.00*10<sup>-6</sup>  </td>
			<td> in/(in* ºF) </td>
		</tr>
		<tr>
			<th> Specific heat capacity </th>
			<td class="centeralign">  452  </td>
			<td> J/(kg*K) </td>
			<td class="centeralign">  0.108  </td>
			<td> BTU/(lb*ºF) </td>
		</tr>
		<tr>
			<th> Thermal conductivity </th>
			<td class="centeralign">  44.7  </td>
			<td> W/(m*K) </td>
			<td class="centeralign">  310  </td>
			<td> BTU*in/(hr*ft²*ºF) </td>
		</tr>
		<tr>
			<th> Electric resistivity </th>
			<td class="centeralign">  2.28*10<sup>-7</sup>  </td>
			<td> Ohm*m </td>
			<td class="centeralign">  2.28*10<sup>-5</sup>  </td>
			<td> Ohm*cm </td>
		</tr>
		<tr>
			<th> Tensile strength (annealed) </th>
			<td class="centeralign">  572  </td>
			<td> MPa </td>
			<td class="centeralign">  83000  </td>
			<td> psi </td>
		</tr>
		<tr>
			<th> Yield strength (annealed) </th>
			<td class="centeralign">  293  </td>
			<td> MPa </td>
			<td class="centeralign">  42500  </td>
			<td> psi </td>
		</tr>
		<tr>
			<th> Elongation (annealed) </th>
			<td class="centeralign">  29  </td>
			<td> % </td>
			<td class="centeralign">  29  </td>
			<td> % </td>
		</tr>
		<tr>
			<th> Hardness (annealed) </th>
			<td class="centeralign">  85  </td>
			<td> RB </td>
			<td class="centeralign">  85  </td>
			<td> RB </td>
		</tr>
		<tr>
			<th> Tensile strength (normalized) </th>
			<td class="centeralign">  793  </td>
			<td> MPa </td>
			<td class="centeralign">  115000  </td>
			<td> psi </td>
		</tr>
		<tr>
			<th> Yield strength (normalized) </th>
			<td class="centeralign">  472  </td>
			<td> MPa </td>
			<td class="centeralign">  68500  </td>
			<td> psi </td>
		</tr>
		<tr>
			<th> Elongation (normalized) </th>
			<td class="centeralign">  23  </td>
			<td> % </td>
			<td class="centeralign">  23  </td>
			<td> % </td>
		</tr>
		<tr>
			<th> Hardness (normalized) </th>
			<td class="centeralign">  98  </td>
			<td> RB </td>
			<td class="centeralign">  98  </td>
			<td> RB</td>
		</tr>
	</tbody>
</table>
]]></description>
		<link>http://www.materialpedia.com/content/1/29/en/aisi-sae-5140.html</link>
		<pubDate>Thu, 29 May 2008 22:17:00 GMT</pubDate>
	</item>
	<item>
		<title><![CDATA[SAE AISI 4130 Alloy steel]]></title>
		<description><![CDATA[<h1><a id="alloy_steel_sae_4130" name="alloy_steel_sae_4130"></a>Alloy steel SAE 4130</h1>
<p>
(submitted by the website administration)<br />
<br />
</p>
<table border="0" class="inline">
	<tbody>
		<tr>
			<td class="centeralign" colspan="5">  <strong>SAE 4130</strong>  </td>
		</tr>
		<tr>
			<td colspan="5"> <strong>Chemical composition: </strong>C=0.30%, Mn=0.5%, Mo=0.20%, Cr=1.0% </td>
		</tr>
		<tr>
			<td> <strong>Property</strong> </td>
			<td colspan="2"> <strong>Value in metric unit</strong> </td>
			<td colspan="2"> <strong>Value in </strong><strong>US</strong><strong> unit</strong> </td>
		</tr>
		<tr>
			<th> Density </th>
			<td class="centeralign">  7.872 *10³  </td>
			<td> kg/m³ </td>
			<td class="centeralign">  491.4  </td>
			<td> lb/ft³ </td>
		</tr>
		<tr>
			<th> Modulus of elasticity </th>
			<td class="centeralign">  205  </td>
			<td> GPa </td>
			<td class="centeralign">  29700  </td>
			<td> ksi </td>
		</tr>
		<tr>
			<th> Thermal expansion (20 ºC) </th>
			<td class="centeralign">  11.2*10<sup>-6</sup>  </td>
			<td> ºC&#713;¹ </td>
			<td class="centeralign">  6.20*10<sup>-6</sup>  </td>
			<td> in/(in* ºF) </td>
		</tr>
		<tr>
			<th> Specific heat capacity </th>
			<td class="centeralign">  477  </td>
			<td> J/(kg*K) </td>
			<td class="centeralign">  0.114  </td>
			<td> BTU/(lb*ºF) </td>
		</tr>
		<tr>
			<th> Thermal conductivity </th>
			<td class="centeralign">  42.7  </td>
			<td> W/(m*K) </td>
			<td class="centeralign">  296  </td>
			<td> BTU*in/(hr*ft²*ºF) </td>
		</tr>
		<tr>
			<th> Electric resistivity </th>
			<td class="centeralign">  2.23*10<sup>-7</sup>  </td>
			<td> Ohm*m </td>
			<td class="centeralign">  2.23*10<sup>-5</sup>  </td>
			<td> Ohm*cm </td>
		</tr>
		<tr>
			<th> Tensile strength (annealed) </th>
			<td class="centeralign">  561  </td>
			<td> MPa </td>
			<td class="centeralign">  81300  </td>
			<td> psi </td>
		</tr>
		<tr>
			<th> Yield strength (annealed) </th>
			<td class="centeralign">  361  </td>
			<td> MPa </td>
			<td class="centeralign">  52300  </td>
			<td> psi </td>
		</tr>
		<tr>
			<th> Elongation (annealed) </th>
			<td class="centeralign">  28  </td>
			<td> % </td>
			<td class="centeralign">  28  </td>
			<td> % </td>
		</tr>
		<tr>
			<th> Hardness (annealed) </th>
			<td class="centeralign">  82  </td>
			<td> RB </td>
			<td class="centeralign">  82  </td>
			<td> RB </td>
		</tr>
		<tr>
			<th> Tensile strength (normalized) </th>
			<td class="centeralign">  669  </td>
			<td> MPa </td>
			<td class="centeralign">  97000  </td>
			<td> psi </td>
		</tr>
		<tr>
			<th> Yield strength (normalized) </th>
			<td class="centeralign">  436  </td>
			<td> MPa </td>
			<td class="centeralign">  63300  </td>
			<td> psi </td>
		</tr>
		<tr>
			<th> Elongation (normalized) </th>
			<td class="centeralign">  25  </td>
			<td> % </td>
			<td class="centeralign">  25  </td>
			<td> % </td>
		</tr>
		<tr>
			<th> Hardness (normalized) </th>
			<td class="centeralign">  93  </td>
			<td> RB </td>
			<td class="centeralign">  93  </td>
			<td> RB</td>
		</tr>
	</tbody>
</table>
]]></description>
		<link>http://www.materialpedia.com/content/1/28/en/sae-aisi-4130-alloy-steel.html</link>
		<pubDate>Thu, 29 May 2008 22:16:00 GMT</pubDate>
	</item>
	<item>
		<title><![CDATA[SAE AISI 8620]]></title>
		<description><![CDATA[<table border="0" cellspacing="0" cellpadding="0" width="100%">
	<tbody>
		<tr>
			<td align="center" bgcolor="#fff0d5"><font face="Arial" size="4" color="#ff8000"><strong>SAE
			8620</strong></font></td>
			<td align="center"> </td>
		</tr>
		<tr>
			<td colspan="3" width="100%" height="20" align="center"> </td>
		</tr>
	</tbody>
</table>
<p>
<font face="Arial"><strong><font color="#ff8000">GENERAL:</font><br />
</strong>A LOW ALLOY CASE HARDENING STEEL</font>
</p>
<p>
<font face="Arial"><strong><font color="#ff8000">USES: </font><br />
</strong>SUITABLE FOR GEARS AND TRANSMITION PARTS</font>
</p>
<table border="0" cellspacing="0" cellpadding="0" width="100%" height="105">
	<tbody>
		<tr>
			<td colspan="5" width="100%" height="18"><font face="Arial" color="#ff8000"><strong>CHEMICAL
			ANALYSIS:</strong> </font></td>
		</tr>
		<tr>
			<td width="20%" height="18" align="center"><font face="Arial">C </font></td>
			<td width="20%" height="18" align="center"><font face="Arial">SI</font></td>
			<td width="20%" height="18" align="center"><font face="Arial">MN</font></td>
			<td width="20%" height="18" align="center"><font face="Arial">S</font></td>
			<td width="20%" height="18" align="center"><font face="Arial">P</font></td>
		</tr>
		<tr>
			<td width="20%" height="18" align="center"><font face="Arial">0.17/0.23 </font></td>
			<td width="20%" height="18" align="center"><font face="Arial">0.15/0.35 </font></td>
			<td width="20%" height="18" align="center"><font face="Arial">060/0.90 </font></td>
			<td width="20%" height="18" align="center"><font face="Arial">0.040 MAX </font></td>
			<td width="20%" height="18" align="center"><font face="Arial">0.035 MAX</font></td>
		</tr>
		<tr>
			<td colspan="5" width="100%" height="18" align="center"> </td>
		</tr>
		<tr>
			<td width="20%" height="18" align="center"><font face="Arial">Cr</font></td>
			<td width="20%" height="18" align="center"><font face="Arial">Ni</font></td>
			<td width="20%" height="18" align="center"><font face="Arial">Mo</font></td>
			<td width="20%" height="18" align="center"> </td>
			<td width="20%" height="18" align="center"> </td>
		</tr>
		<tr>
			<td width="20%" height="15" align="center"><font face="Arial">0.35/0.60</font></td>
			<td width="20%" height="15" align="center"><font face="Arial">0.40/0.70 </font></td>
			<td width="20%" height="15" align="center"><font face="Arial">0.15/0.25</font></td>
			<td width="20%" height="15" align="center"> </td>
			<td width="20%" height="15" align="center"> </td>
		</tr>
	</tbody>
</table>
<table border="0" cellspacing="0" cellpadding="0" width="100%">
	<tbody>
		<tr>
			<td width="100%" height="25">
			<table border="0" cellspacing="0" cellpadding="0" width="100%">
				<tbody>
					<tr>
						<td width="100%" height="15"> </td>
					</tr>
					<tr>
						<td width="100%"><font face="Arial" color="#ff8000"><strong>TYPICAL MECHANICAL
						PROPERTIES: (EXAMPLE ONLY) </strong></font><br />
						<font face="Arial">CARBURISE OR THROUGH HARDEN AS REQUIRED</font></td>
					</tr>
				</tbody>
			</table>
			</td>
		</tr>
	</tbody>
</table>
<p>
<font face="Arial" color="#ff8000"><strong>HEAT TREATMENT &amp; CONDITION<br />
</strong></font><font face="Arial">COMMERCIALY AVAILABLE IN AS ROLLED CONDITION</font>
</p>
<p>
<font face="Arial" color="#ff8000"><strong>SECTIONS<br />
</strong></font><font face="Arial">COMMERCIALY AVAILABLE IN BLACK AND BRIGHT ROUNDS</font>
</p>
<p>
<font face="Arial" color="#ff8000"><strong>RELATED SPECIFICATIONS<br />
</strong></font><font face="Arial">BS 970 805M20(EN362),WERKSTOFF 1.6543,KURZNAME
21NiCrMo22</font>
</p>
]]></description>
		<link>http://www.materialpedia.com/content/1/27/en/sae-aisi-8620.html</link>
		<pubDate>Thu, 29 May 2008 22:13:00 GMT</pubDate>
	</item>
	<item>
		<title><![CDATA[Aluminum Casting]]></title>
		<description><![CDATA[<br />
Aluminum Casting<br />
<br />
Foundries produce complex metal shapes by melting aluminum or aluminum alloys and pouring the molten metal into a mold to solidify into the desired shape. Aluminum casting accounts for 32% of all metal castings in the United States and the majority of these castings are for the automotive industry. There are three main methods used for casting metals: sand casting, investment casting, permanent mold casting, and die casting.<br />
<br />
Die casting and permanent mold casting together account for over 80% of all aluminum casting. Due to aluminum&#39;s low melting temperature, inexpensive steel and iron can be used for forming the dies and molds. The molten aluminum feeding the casting line is derived from three different sources: ingots from a primary aluminum producer, molten aluminum directing from a smelting plant, or partially processed recycled aluminum scrap.<br />
<br />
Casting consists of pouring molten aluminum into molds. Once in the mold, the aluminum solidifies into the shape defined by the mold. Three different casting methods are used: sand casting, permanent mold casting, and die casting. Molten aluminum is derived from three different sources: ingots from a primary aluminum producer, molten aluminum directly from a smelting plant, or partially processed recycled aluminum scrap.<br />
<br />
Sand Casting<br />
<br />
Sand Casting is the most versatile method and the most economical for producing small quantities. Almost any shape mold can be produced from fine sand and binder mixture. After casting, the sand molds must either be hauled to land-fills or reconditioned. Thermal sand reclamation processes are available that remove the binder material from the sand and allow the sand to be reused. These processes are typically natural gas fired.<br />
<br />
Investment Casting<br />
<br />
Investment casting uses a ceramic mold which was created around a plastic or wax replica of the desired metal shape. Prior to casting, the ceramic mold is fired which increases the mold strength and burns the plastic or wax replica, removing it from the mold. Investment casting is capable of creating higher precision casts than sand casting.<br />
<br />
Permanent Mold Casting<br />
<br />
Permanent mold casting uses steel or other metal molds to shape the molten aluminum. Molten aluminum is forced into the mold under gravity or with the aid of a vacuum. Permanent mold castings are stronger than sand castings and less expensive for large production quantities.<br />
<br />
Die Casting<br />
<br />
Die Casting is used for producing accurate components which require little subsequent matching. The molten aluminum is forced under high pressure into steel molds or dies which shape and cool the molten aluminum. 
]]></description>
		<link>http://www.materialpedia.com/content/9/26/en/aluminum-casting.html</link>
		<pubDate>Mon, 31 Mar 2008 12:53:00 GMT</pubDate>
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