ARC-1969-A-16712
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)
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NASA ID
ARC-1969-A-16712
Date Created
December 6, 1951
Center
ARC
Media Type
image
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