updated email name and latest release

Author: planes

.DS_Store

@@ -263,7 +263,7 @@ <h1><font color="red"> The SUAVE Team</font></h1>
 				<table>
 					<tr>
 						<td align="center">
-              <p> Having trouble viewing this email? View it as a <a href="https://suave.stanford.edu/email/email_v2_3.html">webpage.</a></p>
+              <p> Having trouble viewing this email? View it as a <a href="https://suave.stanford.edu/email/email_v230.html">webpage.</a></p>
 
 							<p>SUAVE is maintained by the Aerospace Design Lab in the Department of Aeronautics and Astronautics at Stanford University and is released under an open-source license (LGPL v2.1).
               This list is only used to disseminate important information and updates regarding our software. The development team respects your privacy, and should you wish, you can <a href="https://mailman.stanford.edu/mailman/listinfo/suave-users"><unsubscribe>unsubscribe</unsubscribe></a> from our email list.

email/email_v230.html

@@ -68,34 +68,23 @@
 
 								<article>
 									<header>
-										<h2>SUAVE 2.2.0</h2>
+										<h2>SUAVE 2.3.0</h2>
 										<p>The Latest Evolution in Aerospace Design</p>
 									</header>
 
 									<p>This new version of SUAVE brings a host of upgrades, new features, and improvements to better meet emerging needs in industry, academia, and research. A longer list of improvements can be found below:</p>
 
 
 									<ul>
-									<li>Supersonic Vortex Lattice Method as default aerodynamic method
-									  <ul>
-									    <li>Optimized for quick execution </li>
-									    <li>Able to be used with a surrogate or exact throughout a flight</li> 
-									  </ul>
+									<li>Updates to the native Vortex Lattice Method
 									</li>
-									<li style="margin-top: -32px;">New Plotting</li>	
-									<li>Updated weight methods for transport class vehicles</li>
-									<li>Differential evolution algorithm with constraints</b></li>
-									<li>New algorithm for CG and Mass computations</b></li>
-									<li>Updated OpenVSP interface</li>	
-									<li>import_airfoil_geometry.py now recognizes Selig format airfoil files</b></li>
-									<li>Generalizations for future generative design capabilities</b></li>
-									<li>Bug fixes:
-									   <ul>
-									      <li>ordered data updates </li>
-									      <li>ground segment bug in 2.1  </li>
-									      <li>issues with imports on some Macs</li>
-									      <li>many many more... </li>
-									   </ul>	
+									<li>Propeller-wing interaction modeling</li>	
+									<li>Integrated FLOPS and Raymer aircraft weight estimation methods</li>
+									<li>Improvements to eVTOL networks</b></li>
+									<li>New constant-speed Internal Combustion Engine network</b></li>
+									<li>Lift-trimmed single point segments</li>	
+									<li>Optimized range and endurance speeds for propeller aircraft</b></li>
+									<li>More regressions testing to support our Verification and Validation efforts</b></li>
 									</ul>
 
 									<br>