Updated hyperlinks

Author: cvencro

_tutorials/incompressible_flow/Inc_Turbulent_NACA0012.md

@@ -21,12 +21,12 @@ This tutorial also provides an explanation of the non-dimensional scheme used fo
 
 The resources for this tutorial can be found in the [Inc_Turbulent_NACA0012](https://github.com/su2code/su2code.github.io/tree/master/Inc_Turbulent_NACA0012) directory in the [project website repository](https://github.com/su2code/su2code.github.io). You will need the configuration file ([turb_naca0012.cfg](../../Inc_Turbulent_NACA0012/turb_naca0012.cfg)) and the mesh file ([n0012_897-257.su2](../../Inc_Turbulent_NACA0012/n0012_897-257.su2)).
 
- The 897x257 mesh is obtained from the Langley Research Center Turbulence Modeling Resource (TMR) website, Additionally, skin friction and pressure distribution data for the CFL3D code, along with experiemental pressure data of Gregory (N. Gregory and C. L. O’Reilly. Low-speed aerodynamic characteristics of naca 0012 aerofoil sections, including the effects
+ The 897x257 mesh is obtained from the Langley Research Center Turbulence Modeling Resource (TMR) website, Additionally, skin friction and pressure distribution data for the CFL3D code, along with experimental pressure data of Gregory (N. Gregory and C. L. O’Reilly. Low-speed aerodynamic characteristics of naca 0012 aerofoil sections, including the effects
 of upper-surface roughness simulation hoar frost. NASA R & M 3726, 1970.), from the TMR are used for later comparison with SU2 results. These files can be found on the following website: https://turbmodels.larc.nasa.gov/naca0012_val.html.
 
 ## Tutorial
 
-The following tutorial will walk you through the steps required when solving for the turbulent flow over the NACA 0012 using the incompresible solver in SU2. It is assumed you have already obtained and compiled the SU2_CFD code for a serial computation or both the SU2_CFD and SU2_SOL codes for a parallel computation. If you have yet to complete these requirements, please see the [Download](/docs/Download/) and [Installation](/docs/Installation/) pages.
+The following tutorial will walk you through the steps required when solving for the turbulent flow over the NACA 0012 using the incompresible solver in SU2. It is assumed you have already obtained and compiled the SU2_CFD code for a serial computation or both the SU2_CFD and SU2_SOL codes for a parallel computation. If you have yet to complete these requirements, please see the [Download](../../_docs/Download.md) and [Installation](../../_docs/Installation.md) pages.
 
 ### Background