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