Update Quick-Start.md

Author: talbring

_docs/Quick-Start.md

@@ -7,7 +7,7 @@ permalink: /docs/Quick-Start/
 
 ## Introduction
 
-Welcome to the Quick Start Tutorial for the SU2 software suite. This tutorial is intended to demonstrate some of the key features of the analysis and design tools in an easily accessible format. Completion of this tutorial only requires a few minutes. If you haven't done so already, please visit the [Download](/docs/Download/) and [Installation](/docs/Installation/) pages to obtain the most recent stable release of the software and details for installation. This tutorial requires only the SU2_CFD tool from the SU2 suite.
+Welcome to the Quick Start Tutorial for the SU2 software suite. This tutorial is intended to demonstrate some of the key features of the analysis and design tools in an easily accessible format. Completion of this tutorial only requires a few minutes. If you haven't done so already, please visit the [Download](/download.html) and [Installation](/docs/Installation/) pages to obtain the most recent stable release of the software and details for installation. This tutorial requires only the SU2_CFD tool from the SU2 suite.
 
 ## Goals
 Upon completing this simple tutorial, the user will be familiar with performing the flow and continuous adjoint simulation of external, inviscid flow around a 2D geometry and be able to plot both the flow solution and the surface sensitivities that result. The specific geometry chosen for the tutorial is the NACA 0012 airfoil. Consequently, the following capabilities of SU2 will be showcased in this tutorial:
@@ -24,7 +24,7 @@ The files necessary to run this tutorial are included in the SU2/QuickStart/ dir
 
 ## Tutorial
 
-The following tutorial will walk you through the steps required to compute the flow and adjoint solutions around the NACA 0012 airfoil using SU2. Again, we assume that you have already obtained and compiled the SU2_CFD code (either individually, or as part of the complete SU2 package) for a serial computation. If you have yet to complete this requirement, please see the [Download](/docs/Download/) and [Installation](/docs/Installation) pages.
+The following tutorial will walk you through the steps required to compute the flow and adjoint solutions around the NACA 0012 airfoil using SU2. Again, we assume that you have already obtained and compiled the SU2_CFD code (either individually, or as part of the complete SU2 package) for a serial computation. If you have yet to complete this requirement, please see the [Download](/download.html) and [Installation](/docs/Installation) pages.
 
 ### Background
 
@@ -120,4 +120,4 @@ Figure (4): Contours of the adjoint density variable.
 
 Figure (5): Surface sensitivities. The surface sensitivity is the change in the objective function due to an infinitesimal deformation of the surface in the local normal direction. These values are calculated at each node on the airfoil surface from the flow and adjoint solutions at negligible computational cost using an additional step not described in this tutorial.
 
-Congratulations! You've successfully performed your first flow simulations with SU2. Move on to the [tutorials](https://su2code.github.io/Tutorials/) to learn much more about using the code, and don't forget to read through the information in the user's guide. Having problems with the quick start or visualizing the results?  Visit the [FAQs](/docs/FAQ) page, or see our forum at [CFD-online](http://www.cfd-online.com/Forums/su2/).
+Congratulations! You've successfully performed your first flow simulations with SU2. Move on to the [tutorials](https://su2code.github.io/tutorials/home) to learn much more about using the code, and don't forget to read through the information in the user's guide. Having problems with the quick start or visualizing the results?  Visit the [FAQs](/docs/FAQ) page, or see our forum at [CFD-online](http://www.cfd-online.com/Forums/su2/).