BOUNDARY-LAYER TRANSITION MEASUREMENTS ON A BLUNT OGIVE AT MACH 6


In partnership with Purdue University, the U.S. Air Force and Navy, this project advances fundamental understandings of boundary-layer transition, which is critical for hypersonic vehicle design, through testing, modeling, simulations, and high-performance computing.




Resources: Google Drive | OneDrive | Teams Sharepoint

Software: BLT "Harris" Code (Github, Manual )

Chat: Slackchannel (mu2com)

Computing: Microsoft Azure | Cloudshell