nice a12 stroker A14 crank or A15?
anyone have sounds of this?
http://en.wikipedia.org/wiki/Chrysler_IV-2220General characteristics
Type: 16-cylinder turbo-supercharged liquid-cooled 60° inverted V aircraft piston engine
Bore: 5.8 in (147.3 mm)
Stroke: 5.25 in (133.4 mm)
Displacement: 2,219 cu in (36.36 l)
Length: 122 in (3,098.8 mm)
Width: 33.5 in (850.9 mm)
Height: 33.5 in (850.9 mm)
Dry weight: 2,430 lb (1,102.2 kg)
Components
Valvetrain: Single overhead camshaft actuating two valves per cylinder
Supercharger: With aftercooler
Turbocharger: With water-to-air intercooler
Fuel system: 1 x Bedix-Stromberg PD-16D1 2-barrel horizontal injection carburettor with automatic mixture control
Fuel type: 100/130 grade gasoline
Oil system: Pressure fed at 70 psi (482,633.0 Pa), dry sump, 120 S.U. (25.1 cs) grade oil.
Cooling system: Liquid-cooled
Performance
Power output:
2,500 hp (1,864.2 kW) at 3,400 rpm for takeoff
2,500 hp (1,864.2 kW) at 25,000 ft (7,620 m) METO
2,150 hp (1,603.3 kW) at 3,200 rpm normal rating
1,450 hp (1,081.3 kW) at 2,800 rpm cruise
Specific power: 1.13 hp/cu in (51.2 kW/L)
Compression ratio: 6.3:1
Fuel consumption: 0.42 lb/hp/hr (0.2555 kg/kW/hr)
Specific fuel consumption:
0.54 lb/(hp·h) (0.33 kg/kW/hr)) METO
0.43 lb/(hp·h) (0.26 kg/kW/hr)) normal rating
Oil consumption: 0.005 lb/hp/h (0.003 kg/kW/hr)
Power-to-weight ratio: 1.02 hp/lb (1.84 kW/kg)
Transfer
