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The Vought XF5U "Flying Flapjack" was an experimental U.S. Navy fighter aircraft designed by Charles H. Zimmerman for Vought during World War II. This unorthodox design consisted of a flat, somewhat disc-shaped body (hence its name) serving as the lifting surface.[1] Two piston engines buried in the body drove propellers located on the leading edge at the wingtips.

Not to be confused with Grumman XF5F Skyrocket.
XF5U
The XF5U-1 during testing
Role Fighter
Manufacturer Vought
Designer Charles H. Zimmerman
First flight 1943
Status Cancelled 17 March 1947
Primary user United States Navy
Number built 2
Developed from Vought V-173

Design and development


A developed version of the original V-173 prototype, the XF5U-1 was a larger aircraft. Of all-metal construction, it was almost five times heavier, with two 1,400 hp (1,193 kW) Pratt & Whitney R-2000 radial engines. The configuration was designed to create a low aspect ratio aircraft with low takeoff and landing speeds but high top speed.[2] The aircraft was designed to keep the low stall speed and high angle of attack from the V-173 prototype while providing for better pilot visibility, cockpit comfort, less vibration, and provisions to install armament. This included a cockpit redesign moving the cockpit from the leading edge of the wing to a nose nacelle that extended further in front of the leading edge. The arrestor hook was changed to a dorsal hook that would diminish the drag from the apparatus.[3]

XF5U-1 cockpit
XF5U-1 cockpit

Normally, a wing with such a low aspect ratio will suffer from very poor performance due to the degree of induced drag created at the wingtips, as the higher pressure air below spills around the wingtip to the lower-pressure region above. In a conventional aircraft, these wingtip vortices carry a lot of energy with them and hence create drag. The usual approach to reducing these vortices is to build a wing with a high aspect ratio, i.e. one that is long and narrow. However, such wings compromise the maneuverability and roll rate of the aircraft, or present a structural challenge in building them stiff enough. The XF5U attempted to overcome the tip vortex problem using the propellers to actively cancel the drag-causing tip vortices.[4] The propellers are arranged to rotate in the opposite direction to the tip vortices, with the aim of retaining the higher-pressure air below the wing. With this source of drag eliminated, the aircraft would fly with a much smaller wing area, and the small wing would yield high maneuverability with greater structural strength.

The propellers envisioned for the completed fighter — unlike the torque-reducing counter-rotating propellers of the V-173 design — were to have a built-in cyclic movement like a helicopter's main rotor, with a very limited ability to shift their center of lift up and down to aid the aircraft in maneuvering. Initially, the aircraft used propellers originally designed for the V-173 prototype.[5] These propellers would be replaced with propellers taken from the Vought F4U-4 Corsair. An ejection seat was fitted to allow the pilot to clear the massive propellers in the event of an in-flight emergency.[2] Although the prototype was unarmed, a combination of six M2 Browning 50-caliber machine guns or four M3 20 mm cannons would be mounted in the wing roots in service.[2]


Testing and evaluation


The XF5U design was promising: specifications given at the time promised great maneuverability and speeds up to 452 mph (727 km/h).[6] However, it came at the time when the United States Navy was switching from propeller driven to jet propelled aircraft. By 1946, the XF5U-1 project was already long over its expected development time, and well over budget.[2] With jet aircraft coming into service, the Navy finally canceled the project on 17 March 1947, and the prototype aircraft (V-173) was transferred to the Smithsonian Museum for display. Although two aircraft were constructed, a lone XF5U-1 underwent ground runs but never overcame vibration problems. Taxi trials at Vought's Connecticut factory culminated in short "hops" that were not true flights.[7][8] The only completed XF5U-1 proved to be so structurally solid that it had to be destroyed with a wrecking ball.[9]


Specifications (XF5U-1)


3-view line drawing of the Vought XF5U
3-view line drawing of the Vought XF5U

General characteristics

Performance

Armament


See also


Related development

Aircraft of comparable role, configuration, and era

Related lists


References



Notes


  1. Chant 1984, p. 53.
  2. Winchester Concept Aircraft 2005, p. 247.
  3. Naval Fighters Number Twenty One Chance Vought V-173 and Xf5U-1 Flying Pancakes. Steve Ginter. 1992. pp. 15, 23.
  4. Norton 2008, p.165
  5. Naval Fighters Number Twenty One Chance Vought V-173 and Xf5U-1 Flying Pancakes. Steve Ginter. 1992. p. 15.
  6. http://www.ibiblio.org/hyperwar/USN/SAC/XF5U-1_FlapjackACP-440601.pdf [bare URL PDF]
  7. Winchester X-Planes 2005, p. 222. Suggestions of first XF5U flight were confused the V-173 test flying that continued into 1945.
  8. Jerram 1980, p. 71.
  9. Jerram 1980, p. 72.

Bibliography




Wikimedia Commons has media related to Vought XF5U.

На других языках

[de] Chance Vought XF5U

Die Chance Vought XF5U (Werksbezeichnung VS-315) war der Prototyp eines geplanten extrem kurzstartfähigen Jagdflugzeugs des US-amerikanischen Herstellers Chance Vought aus den 1940er Jahren. Der inoffizielle Beiname Flying Flapjack (Fliegender Pfannkuchen) rührt von der ungewöhnlichen konstruktiven Auslegung mit einer angenähert kreisförmigen Tragfläche her. Die Entwicklung der XF5U basierte auf den Ergebnissen des Erprobungsträgers Chance Vought V-173. Nachdem bereits die V-173 inoffiziell als „Zimmer-Skimmer“ (nach ihrem Konstrukteur Charles H. Zimmerman) bezeichnet wurde, trug die XF5U auch den Beinamen „Skimmer“.
- [en] Vought XF5U

[fr] Vought XF5U

Le Vought XF5U Flying Pancake (Crêpe volante) est un avion de chasse expérimental destiné à l'US Navy, conçu par Charles H. Zimmerman durant la Seconde Guerre mondiale. Il tire son surnom de sa forme peu orthodoxe, la majeure partie de la surface portante étant en forme de disque arrondi[1].

[it] Vought XF5U

Il Vought XF5U era un aereo da caccia con caratteristiche STOL progettato dall'azienda aeronautica statunitense Vought nella prima metà degli anni quaranta.

[ru] Vought XF5U

Vought XF5U-1 Flying Pancake (англ. flying pancake — «Летающий блин») — экспериментальный палубный истребитель, исследовавшийся флотом США во время Второй мировой войны.


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