From the Planes You’ve (Probably) Never Heard Of Department of Wingspan, we bring you the Curtiss XF13C.
The decade of the 1930s was a fascinating time of rapid aircraft development that was marked by the inexorable change from the biplane to the monoplane. Biplanes had been around since the Wright Brothers (though other pioneers famously went the monoplane route), and the two-wing arrangement does benefit from greater lift, better slow speed handling, and more maneuverability when compared to early monoplanes. For that reason, biplanes are still common today. But the monoplane, by ditching one wing and all the attendant struts and bracing wires, is an aerodynamically cleaner design, and less drag generally means more speed. With both layouts showing their own benefits (and drawbacks), it became a question of which flying characteristic was deemed more desirable in an era of transition. But what if you could have both a biplane and a monoplane in the same aircraft? Then, with a few simple steps, you could transition from one to the other. That is exactly what Curtiss attempted to do with the XF13C, known to Curtiss as the Model 70.
At a time when the US Navy was transitioning from its last biplane fighter (Grumman F3F) to its first monoplane fighter (Brewster F2A Buffalo), America’s ocean-going force thought it might be possible to have one plane that would be the best of both worlds: a biplane, whose slower landing speeds and greater lift made it ideal for carrier duty, and a monoplane that could operate from longer land-based runways and enjoy a higher speed. So the XF13C was designed to have a removable lower wing which could be could be used or not, depending on where it would be operating. As a monoplane (XF13C-1), the permanent top wing was mounted on the top of the canopy, and its supporting struts fit into the same mounting points where the detachable lower wing would mount in the biplane configuration (XF13C-2). The only significant drawback was poor pilot visibility, since the pilot’s head was squarely between the upper wings.
The XF13C took its maiden flight on January 7, 1934 in biplane configuration and subsequent flights evaluated the monoplane configuration. As expected, the biplane had a shorter takeoff run, but the landing speed of the of the monoplane, with its leading and trailing edge slats, was only marginally faster, though its takeoff run was considerably longer. By all accounts, the aircraft was stable and had good flying characteristics, though the US Army’s evaluation of the XF13C found it wholly unsuitable for any military use. Carrier evaluations were carried out on the USS Saratoga (CV 3), where it performed acceptably.
After testing, Curtiss took the Navy’s recommendations in hand and gave the quick-change fighter heavier armament, a larger vertical stabilizer, and a more powerful experimental Wright XR-1510 engine which increased top speed slightly. Testing of the newly-dubbed XFC13-3 continued, but the engine proved problematic, and newer aircraft, even newer biplanes, were demonstrating better overall performance. In the end the innovative aircraft was passed to NACA for more testing, and it finished its days in US Marine Corps service as a utility aircraft before being retired and dismantled in 1938.