| 词条 | Arsenal O.101 | |||||||||||||||
| 释义 |
The Arsenal O.101 was a French research aircraft that flew shortly after World War II. It was a low-wing monoplane of conventional configuration with fixed tailwheel undercarriage, but incorporated several novel features for its role as an airborne testbed for evaluating airfoil sections and control surface designs. It was designed to accommodate a pilot and an observer in tandem cockpits. However, since the observer was to be watching the aircraft's wings, this cockpit was sunken fully into the fuselage, affording no fore-and-aft view at all. The pilot's cockpit was set well back along the fuselage, near the tail. The O.101 was fitted with extensive instrumentation to measure pressures and loads throughout the aircraft, and was given dimensions such that the entire aircraft could be placed inside the wind tunnel at Chalais-Meudon without any disassembly required. Specifications{{aerospecs|met or eng?=met |ref= |crew=two, pilot and observer |capacity= |length m=7.60 |length ft=25 |length in=0 |span m=8.25 |span ft=27 |span in=1 |height m=3.20 |height ft=10 |height in=6 |wing area sqm=8.8 |wing area sqft=95 |empty weight kg= |empty weight lb= |gross weight kg=1,730 |gross weight lb=3,810 |eng1 number=1 |eng1 type=Renault 12S piston engine |eng1 kw=370 |eng1 hp=495 |eng2 number= |eng2 type= |eng2 kw= |eng2 hp= |max speed kmh=450 |max speed mph=280 |cruise speed kmh= |cruise speed mph= |range km= |range miles= |endurance h= |endurance min= |ceiling m=8,000 |ceiling ft=26,200 |climb rate ms= |climb rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }} References{{commons category|Arsenal de l'aéronautique}}
|related= |similar aircraft= |sequence= |lists= |see also= }}{{Arsenal de l'Aéronautique}}{{aero-1940s-stub}} 4 : French experimental aircraft 1940–1949|Arsenal aircraft|Single-engined tractor aircraft|Low-wing aircraft |
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