Merge branch 'master' of https://github.com/suavecode/suavecode.github.io

Author: planes

index.html

@@ -88,7 +88,7 @@ <h2>SUAVE 2.4: Faster than before!</h2>
 								<div class="box highlight">
 									<i class="icon major fa-plane"></i>
 									<h3>Open Source</h3>
-									<p>Released in LGPL 2.1. The open source license
+									<p>Released in LGPL 2.1. This open source license
 									enables commercial industry and academia to collaborate together.</p>
 								</div>
 
@@ -184,4 +184,4 @@ <h3>External Links</h3>
 			<script src="assets/js/main.js"></script>
 
 	</body>
-</html>
+</html>

latest_release.html

@@ -68,23 +68,26 @@
 
 								<article>
 									<header>
-										<h2>SUAVE 2.3.0</h2>
+										<h2>SUAVE 2.4.0</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>
+									<p>This release has major changes to both the aerodynamics, acoustics, and propeller models in SUAVE. A longer list of improvements can be found below:</p>
 
 
 									<ul>
-									<li>Updates to the native Vortex Lattice Method
-									</li>
-									<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>
+									<li>New VORLAX-based supersonic VLM</li>
+									<li>Aircraft Noise Analysis</li>	
+									<li>General VTOL weights buildup</li> 
+									<li>Electric performance diagrams</li> 
+									<li>Non-uniform inflow for BET analysis </li> 
+									<li>Updated propeller-wing interaction </li> 
+									<li>Direct use of polar data for propellers</li> 
+									<li>Interface to PyCycle</li> 	
+									<li>Airfoil Interpolator</li>
+									<li>New function for supersonic wave drag</li>
+									<li>Update OpenVSP interface</li>
+									<li>Bug Fixes, code clean up, and some speedups!</li> 
 									</ul>
 
 									<br>
@@ -158,4 +161,4 @@ <h3>External Links</h3>
 			<script src="assets/js/main.js"></script>
 
 	</body>
-</html>
+</html>

publications.html

@@ -65,6 +65,10 @@
 						<div id="content">
 							<!-- Content -->
 							<div class="row">
+								<div class="col-4 col-6-medium col-12-small">
+									<a href="publications/Low_Cost_Aero_Analysis.pdf" class="image fit"><img src="publications/Low_Cost_Aero_Analysis.png" alt=""></a>
+									<p>A Low-Cost Aero-Propulsive Analysis of Distributed Electric Propulsion Aircraft</p>                          
+								</div>
 								<div class="col-4 col-6-medium col-12-small">
 									<a href="publications/AIAA_Propulsion_SUAVE_NDARC_Comparison.pdf" class="image fit"><img src="publications/Aviation_Propulsion_SUAVE_NDARC.PNG" alt=""></a>
 									<p>Current Capabilities and Challenges of NDARC and SUAVE for eVTOL Aircraft Design and Analysis</p>