YF-93
From Warlike
Q2050576
The North American YF-93 was an American fighter development of the F-86 Sabre that emerged as a radically different variant that received its own designation. Two were built and flown before the project was eventually canceled.
Wikimedia, Wikidata
North American YF-93
North American Aviation, Canada, 
Avia BH-8, Aviatik D.VI, Lockheed YP-24, Sukhoi Su-1, Sukhoi Su-3,
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Location: KML, Cluster Map, Maps,
North American F-93 in flight
North American YF-93A on lakebed
NAA YF-93A cutaway
North American F-93 -1 48-317NAA YF-93A cutaway
North American F-93
YF-93A (AF48-318 NACA-151) Flight evaluation and comparison of a NACA submerged inlet and a scoop inlet. The YF-93A's were the first aircraft to use flush NACA engine inlets.
Flight evaluation and comparison of a NACA submerged inlet and a scoop inlet on the North American YF-93A (AF48-317 NACA-139). The YF-93A's were the first aircraft to use flush NACA engine inlets. aircraft to use flush NACA engine inlets.
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.| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | North American F-93 in flight | Commons | ||
| commons | image | North American YF-93A on lakebed | Commons | ||
| commons | image | NAA YF-93A cutaway | Commons | ||
| commons | image | North American F-93 -1 48-317 | Commons | ||
| commons | image | NAA YF-93A cutaway | Commons | ||
| commons | image | North American F-93 | Commons | ||
| commons | image | YF-93A (AF48-318 NACA-151) Flight evaluation and comparison of a NACA submerged inlet and a scoop inlet. The YF-93A's were the first aircraft to use flush NACA engine inlets. | Commons | ||
| commons | image | Flight evaluation and comparison of a NACA submerged inlet and a scoop inlet on the North American YF-93A (AF48-317 NACA-139). The YF-93A's were the first aircraft to use flush NACA engine inlets. aircraft to use flush NACA engine inlets. | Commons | ||
| commons | image | 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. | Commons | ||
