What is it about?
This paper summarizes part of characterization work done on the newly built Mach 6 pulsed arcjet tunnel of the University of Tennessee. In particular, the experiments reported here are related to the intrusive characterization of the tunnel performance and freestream using pitot and heat flux probes.
Featured Image
Read the Original
This page is a summary of: Characterization of University of Tennessee High-Enthalpy Tunnel with Nitrogen Flow, Journal of Thermophysics and Heat Transfer, July 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.t7019.
You can read the full text:
Contributors
Be the first to contribute to this page
