A High-Temperature, Steady-Flow, Supersonic Tunnel

• 1 October 1959
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
• Vol. 26  (10) , 676-677
• https://doi.org/10.2514/8.8252

Abstract

Keywords

• HIGH TEMPERATURE
• SUPERSONIC TUNNEL
• STEADY FLOW