Public domain
ARC-1969-A-16712
From the collection of NASA Image and Video Library. Free to download, adapt and use — no permission needed.
About this work
Date: Dec 6, 1951 NACA Photographer North American YF-93 with submerged divergent-wall engine-air inlet. Maximum high-speed capability of Mach 1.03 was obtained with afterbrner on. Tests were conducted to compare high-speed performance of the YF-93 NACA-139 airplane with different inlet configurations. (Mar 1953)
NASA Image and Video Library’s own descriptionSubjects
Credit lineARC-1969-A-16712. NASA/ARC, 1951-12-06. Public domain. ID: ARC-1969-A-16712.
