Public domain
Multi-Nozzle Base Flow Model in the 10- by 10-Foot Supersonic Wind Tunnel
From the collection of NASA Image and Video Library. Free to download, adapt and use — no permission needed.
About this work
Researchers check the setup of a multi-nozzle base flow model in the 10- by 10-Foot Supersonic Wind Tunnel at the National Aeronautics and Space Administration (NASA) Lewis Research Center. NASA researchers were struggling to understand the complex flow phenomena resulting from the use of multiple rocket engines.
NASA Image and Video Library’s own descriptionCredit lineMulti-Nozzle Base Flow Model in the 10- by 10-Foot Supersonic Wind Tunnel. NASA/GRC, 1964-02-23. Public domain. ID: GRC-1964-C-68368.
